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Documentation
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Documentation
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Main class for defining the problem; basically this class reads the configuration file, and stores all the information. More...
#include <CConfig.hpp>
Public Member Functions | |
| CConfig (char case_filename[MAX_STRING_SIZE], SU2_COMPONENT val_software, bool verb_high) | |
| Constructor of the class which reads the input file. More... | |
| CConfig (istream &case_buffer, SU2_COMPONENT val_software, bool verb_high) | |
| Constructor of the class which takes an istream buffer containing the config options. More... | |
| CConfig (CConfig *config, char case_filename[MAX_STRING_SIZE], SU2_COMPONENT val_software, unsigned short val_iZone, unsigned short val_nZone, bool verb_high) | |
| Constructor of the class which reads the input file and uses default options from another config. More... | |
| CConfig (char case_filename[MAX_STRING_SIZE], SU2_COMPONENT val_software) | |
| Constructor of the class which reads the input file. More... | |
| CConfig (char case_filename[MAX_STRING_SIZE], CConfig *config) | |
| Constructor of the class which reads the input file. More... | |
| ~CConfig (void) | |
| Destructor of the class. More... | |
| void | Init () |
| Initialize common fields of the config structure. More... | |
| void | SetnZone () |
| Set the number of zones. More... | |
| void | SetnDim () |
| Set the physical dimension of the problem. More... | |
| void | SetHeader (SU2_COMPONENT val_software) const |
| Print the header to screen. More... | |
| SU2_MPI::Comm | GetMPICommunicator () const |
| Get the MPI communicator of SU2. More... | |
| void | SetMPICommunicator (SU2_MPI::Comm Communicator) |
| Set the MPI communicator for SU2. More... | |
| void | SetPointersNull (void) |
| Initializes pointers to null. More... | |
| bool | TokenizeString (string &str, string &option_name, vector< string > &option_value) |
| breaks an input line from the config file into a set of tokens More... | |
| std::array< su2double, 3 > | GetRefOriginMoment (unsigned short val_marker) const |
| Get reference origin for moment computation. More... | |
| su2double | GetRefOriginMoment_X (unsigned short val_marker) const |
| Get reference origin x-coordinate for moment computation. More... | |
| su2double | GetRefOriginMoment_Y (unsigned short val_marker) const |
| Get reference origin y-coordinate for moment computation. More... | |
| su2double | GetRefOriginMoment_Z (unsigned short val_marker) const |
| Get reference origin z-coordinate for moment computation. More... | |
| void | SetRefOriginMoment_X (unsigned short val_marker, su2double val_origin) |
| Set reference origin x-coordinate for moment computation. More... | |
| void | SetRefOriginMoment_Y (unsigned short val_marker, su2double val_origin) |
| Set reference origin y-coordinate for moment computation. More... | |
| void | SetRefOriginMoment_Z (unsigned short val_marker, su2double val_origin) |
| Set reference origin z-coordinate for moment computation. More... | |
| string | GetPlaneTag (unsigned short index) const |
| Get index of the upper and lower horizontal plane. More... | |
| su2double | GetEA_IntLimit (unsigned short index) const |
| Get the integration limits for the equivalent area computation. More... | |
| su2double | GetEA_ScaleFactor (void) const |
| Get the integration limits for the equivalent area computation. More... | |
| su2double | GetAdjointLimit (void) const |
| Get the limit value for the adjoint variables. More... | |
| const su2double * | GetHold_GridFixed_Coord (void) const |
| Get the coordinates where of the box where the grid is going to be deformed. More... | |
| const su2double * | GetSubsonicEngine_Values (void) const |
| Get the values of subsonic engine. More... | |
| const su2double * | GetSubsonicEngine_Cyl (void) const |
| Get the cycle of a subsonic engine. More... | |
| const su2double * | GetDistortionRack (void) const |
| Get the distortion rack. More... | |
| unsigned short | GetGeo_Description (void) const |
| Get Description of the geometry to be analyzed. More... | |
| bool | GetExtraOutput (void) const |
| Creates a tecplot file to visualize the partition made by the DDC software. More... | |
| long | GetExtraHeatOutputZone (void) const |
| Heat solver zone with extra screen output. More... | |
| su2double | GetMach (void) const |
| Get the value of the Mach number (velocity divided by speed of sound). More... | |
| su2double | GetGamma (void) const |
| Get the value of the Gamma of fluid (ratio of specific heats). More... | |
| su2double | GetConfinement_Param (void) const |
| Get the value of the Confinement Parameter. More... | |
| su2double | GetCFL_AdaptParam (unsigned short val_index) const |
| Get the values of the CFL adaption parameters. More... | |
| bool | GetCFL_Adapt (void) const |
| Get the value of the CFL adaption flag. More... | |
| su2double | GetStations_Bounds (unsigned short val_var) const |
| Get the value of the limits for the sections. More... | |
| su2double | GetFFD_Axis (unsigned short val_var) const |
| Get the value of the vector that connects the cartesian axis with a sherical or cylindrical one. More... | |
| su2double | GetBulk_Modulus (void) const |
| Get the value of the bulk modulus. More... | |
| su2double | GetBeta_Factor (void) const |
| Get the epsilon^2 multiplier for Beta in the incompressible preconditioner. More... | |
| su2double | GetGas_Constant (void) const |
| Get the value of specific gas constant. More... | |
| su2double | GetGas_ConstantND (void) const |
| Get the value of specific gas constant. More... | |
| su2double | GetMolecular_Weight (unsigned short val_index=0) const |
| Get the value of the molecular weight for an incompressible ideal gas (g/mol). More... | |
| su2double | GetSpecific_Heat_Cp (unsigned short val_index=0) const |
| Get the value of specific heat at constant pressure. More... | |
| su2double | GetSpecific_Heat_CpND (unsigned short val_index=0) const |
| Get the non-dimensional value of specific heat at constant pressure. More... | |
| su2double | GetWallTemperature (void) const |
| Get the value of wall temperature. More... | |
| su2double | GetPnormHeat (void) const |
| Get the p-norm for heat-flux objective functions (adjoint problem). More... | |
| su2double | GetGas_Constant_Ref (void) const |
| Get the reference value for the specific gas constant. More... | |
| su2double | GetHeat_Flux_Ref (void) const |
| Get the reference value for the heat flux. More... | |
| su2double | GetTemperature_FreeStream (void) const |
| Get the value of the freestream temperature. More... | |
| su2double | GetTemperature_ve_FreeStream (void) const |
| Get the value of the freestream vibrational-electronic temperature. More... | |
| su2double | GetEnergy_FreeStream (void) const |
| Get the value of the freestream energy. More... | |
| su2double | GetViscosity_FreeStream (void) const |
| Get the value of the freestream viscosity. More... | |
| su2double | GetDensity_FreeStream (void) const |
| Get the value of the freestream density. More... | |
| su2double | GetModVel_FreeStream (void) const |
| Get the magnitude of the free-stream velocity of the fluid. More... | |
| su2double | GetModVel_FreeStreamND (void) const |
| Get the non-dimensional magnitude of the free-stream velocity of the fluid. More... | |
| su2double | GetPrandtl_Lam (unsigned short val_index=0) const |
| Get the value of the laminar Prandtl number. More... | |
| su2double | GetPrandtl_Turb (unsigned short val_index=0) const |
| Get the value of the turbulent Prandtl number. More... | |
| su2double | GetwallModel_Kappa () const |
| Get the value of the von Karman constant kappa for turbulence wall modeling. More... | |
| unsigned short | GetwallModel_MaxIter () const |
| Get the value of the max. number of Newton iterations for turbulence wall modeling. More... | |
| su2double | GetwallModel_RelFac () const |
| Get the value of the relaxation factor for turbulence wall modeling. More... | |
| su2double | GetwallModel_MinYPlus () const |
| Get the value of the minimum Y+ value below which the wall function is deactivated. More... | |
| su2double | GetwallModel_B () const |
| Get the value of the wall model constant B for turbulence wall modeling. More... | |
| su2double | GetThermalDiffusivity (void) const |
| Get the value of the thermal diffusivity for solids. More... | |
| su2double | GetLength_Ref (void) const |
| Get the value of the reference length for non-dimensionalization. This value should always be 1 internally, and is not user-specified. More... | |
| su2double | GetPressure_Ref (void) const |
| Get the value of the reference pressure for non-dimensionalization. More... | |
| su2double | GetEnergy_Ref (void) const |
| Get the value of the reference energy for non-dimensionalization. More... | |
| su2double | GetTemperature_Ref (void) const |
| Get the value of the reference temperature for non-dimensionalization. More... | |
| su2double | GetTemperature_ve_Ref (void) const |
| Get the value of the reference temperature for non-dimensionalization. More... | |
| su2double | GetDensity_Ref (void) const |
| Get the value of the reference density for non-dimensionalization. More... | |
| su2double | GetVelocity_Ref (void) const |
| Get the value of the reference velocity for non-dimensionalization. More... | |
| su2double | GetTime_Ref (void) const |
| Get the value of the reference time for non-dimensionalization. More... | |
| su2double | GetViscosity_Ref (void) const |
| Get the value of the reference viscosity for non-dimensionalization. More... | |
| su2double | GetHighlite_Area (void) const |
| Get the value of the reference viscosity for non-dimensionalization. More... | |
| su2double | GetFan_Poly_Eff (void) const |
| Get the value of the reference viscosity for non-dimensionalization. More... | |
| su2double | GetThermal_Conductivity_Ref (void) const |
| Get the value of the reference thermal conductivity for non-dimensionalization. More... | |
| su2double | GetOmega_Ref (void) const |
| Get the value of the reference angular velocity for non-dimensionalization. More... | |
| su2double | GetForce_Ref (void) const |
| Get the value of the reference force for non-dimensionalization. More... | |
| su2double | GetPressure_FreeStream (void) const |
| Get the value of the non-dimensionalized freestream pressure. More... | |
| su2double | GetPressure_FreeStreamND (void) const |
| Get the value of the non-dimensionalized freestream pressure. More... | |
| su2double | GetPressure_Thermodynamic (void) const |
| Get the value of the thermodynamic pressure. More... | |
| su2double | GetPressure_ThermodynamicND (void) const |
| Get the value of the non-dimensionalized thermodynamic pressure. More... | |
| su2double * | GetVelocity_FreeStream (void) |
| Get the vector of the dimensionalized freestream velocity. More... | |
| const su2double * | GetVelocity_FreeStream (void) const |
| su2double | GetTemperature_FreeStreamND (void) const |
| Get the value of the non-dimensionalized freestream temperature. More... | |
| su2double | GetTemperature_ve_FreeStreamND (void) const |
| Get the value of the non-dimensionalized vibrational-electronic freestream temperature. More... | |
| su2double | GetDensity_FreeStreamND (void) const |
| Get the value of the non-dimensionalized freestream density. More... | |
| su2double * | GetVelocity_FreeStreamND (void) |
| Get the vector of the non-dimensionalized freestream velocity. More... | |
| const su2double * | GetVelocity_FreeStreamND (void) const |
| su2double | GetEnergy_FreeStreamND (void) const |
| Get the value of the non-dimensionalized freestream energy. More... | |
| su2double | GetViscosity_FreeStreamND (void) const |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetTke_FreeStreamND (void) const |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetOmega_FreeStreamND (void) const |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetTke_FreeStream (void) const |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetOmega_FreeStream (void) const |
| Get the value of the non-dimensionalized freestream viscosity. More... | |
| su2double | GetIntermittency_FreeStream (void) const |
| Get the value of the non-dimensionalized freestream intermittency. More... | |
| su2double | GetReThetaT_FreeStream () const |
| Get the value of the freestream momentum thickness Reynolds number. More... | |
| su2double | GetTurbulenceIntensity_FreeStream (void) const |
| Get the value of the non-dimensionalized freestream turbulence intensity. More... | |
| su2double | GetNuFactor_FreeStream (void) const |
| Get the value of the non-dimensionalized freestream turbulence intensity. More... | |
| su2double | GetKFactor_LowerLimit (void) const |
| Get the k constant factor define a lower limit by multiplication with values in SST turbulence model. More... | |
| su2double | GetOmegaFactor_LowerLimit (void) const |
| Get the w constant factor define a lower limit by multiplication with values in SST turbulencemodel. More... | |
| su2double | GetNuFactor_Engine (void) const |
| Get the value of the non-dimensionalized engine turbulence intensity. More... | |
| su2double | GetSecondaryFlow_ActDisk (void) const |
| Get the value of the non-dimensionalized actuator disk turbulence intensity. More... | |
| su2double | GetInitial_BCThrust (void) const |
| Get the value of the non-dimensionalized actuator disk turbulence intensity. More... | |
| void | SetInitial_BCThrust (su2double val_bcthrust) |
| Get the value of the non-dimensionalized actuator disk turbulence intensity. More... | |
| su2double | GetTurb2LamViscRatio_FreeStream (void) const |
| Get the value of the turbulent to laminar viscosity ratio. More... | |
| su2double | GetLength_Reynolds (void) const |
| Get the value of the Reynolds length. More... | |
| su2double | GetRefArea (void) const |
| Get the reference area for non dimensional coefficient computation. If the value from the is 0 then, the code will compute the reference area using the projection of the shape into the z plane (3D) or the x plane (2D). More... | |
| su2double | GetThermal_Expansion_Coeff (void) const |
| Get the thermal expansion coefficient. More... | |
| su2double | GetThermal_Expansion_CoeffND (void) const |
| Get the non-dim. thermal expansion coefficient. More... | |
| void | SetThermal_Expansion_Coeff (su2double val_thermal_expansion) |
| Set the thermal expansion coefficient. More... | |
| void | SetThermal_Expansion_CoeffND (su2double val_thermal_expansionnd) |
| Set the non-dim. thermal expansion coefficient. More... | |
| su2double | GetInc_Density_Ref (void) const |
| Get the value of the reference density for custom incompressible non-dimensionalization. More... | |
| su2double | GetInc_Velocity_Ref (void) const |
| Get the value of the reference velocity for custom incompressible non-dimensionalization. More... | |
| su2double | GetInc_Temperature_Ref (void) const |
| Get the value of the reference temperature for custom incompressible non-dimensionalization. More... | |
| su2double | GetInc_Density_Init (void) const |
| Get the value of the initial density for incompressible flows. More... | |
| const su2double * | GetInc_Velocity_Init (void) const |
| Get the value of the initial velocity for incompressible flows. More... | |
| su2double | GetInc_Temperature_Init (void) const |
| Get the value of the initial temperature for incompressible flows. More... | |
| bool | GetSpecies_Clipping () const |
| Get the flag for activating species transport clipping. More... | |
| su2double | GetSpecies_Clipping_Max (unsigned short iVar) const |
| Get the maximum bound for scalar transport clipping. More... | |
| su2double | GetSpecies_Clipping_Min (unsigned short iVar) const |
| Get the minimum bound for scalar transport clipping. More... | |
| const su2double * | GetSpecies_Init () const |
| Get initial species value/concentration in the range [0,1]. More... | |
| bool | GetSpecies_StrongBC () const |
| Get the flag for using strong BC's for in- and outlets in the species solver. More... | |
| const su2double * | GetFlameInit () const |
| Get the flame initialization. (x1,x2,x3) = flame offset/spark center location. (x4,x5,x6) = flame normal, separating unburnt from burnt or spark radius, spark start iteration, spark duration. (x7) = flame thickness, the length from unburnt to burnt conditions. (x8) = flame burnt thickness, the length to stay at burnt conditions. More... | |
| const su2double * | GetSpark () const |
| Get species net reaction rates applied during spark ignition. More... | |
| bool | GetPreferentialDiffusion () const |
| Preferential diffusion combustion problem. More... | |
| void | SetPreferentialDiffusion (bool input) |
| Define preferential diffusion combustion problem. More... | |
| unsigned short | GetNControlVars () const |
| Get the number of control variables for flamelet model. More... | |
| unsigned short | GetNScalars () const |
| Get the number of total transported scalars for flamelet model. More... | |
| unsigned short | GetNUserScalars () const |
| Get the number of user scalars for flamelet model. More... | |
| const string & | GetControllingVariableName (unsigned short i_cv) const |
| Get the name of a specific controlling variable. More... | |
| const string & | GetControllingVariableSourceName (unsigned short i_cv) const |
| Get the name of the source term variable for a specific controlling variable. More... | |
| const string & | GetUserScalarName (unsigned short i_user_scalar) const |
| Get the name of the user scalar. More... | |
| const string & | GetUserSourceName (unsigned short i_user_source) const |
| Get the name of the user scalar source term. More... | |
| FLAMELET_INIT_TYPE | GetFlameletInitType () const |
| Get the ignition method used for combustion problems. More... | |
| unsigned short | GetNLookups () const |
| Get the number of transported scalars for combustion. More... | |
| const string & | GetLookupName (unsigned short i_lookup) const |
| Get the name of the variable that we want to retrieve from the lookup table. More... | |
| su2double | GetElasticyMod (unsigned short id_val) const |
| Get the Young's modulus of elasticity. More... | |
| bool | GetDE_Effects (void) const |
| Decide whether to apply DE effects to the model. More... | |
| unsigned short | GetnElectric_Constant (void) const |
| Get the number of different electric constants. More... | |
| su2double | GetElectric_Constant (unsigned short iVar) const |
| Get the value of the DE modulus. More... | |
| su2double | GetKnowles_B (void) const |
| Get the value of the B constant in the Knowles material model. More... | |
| su2double | GetKnowles_N (void) const |
| Get the value of the N constant in the Knowles material model. More... | |
| unsigned short | GetDV_FEA (void) const |
| Get the kind of design variable for FEA. More... | |
| unsigned long | GetRefNode_ID (void) const |
| Get the ID of the reference node. More... | |
| su2double | GetRefNode_Displacement (unsigned short val_coeff) const |
| Get the values for the reference node displacement. More... | |
| su2double | GetRefNode_Penalty (void) const |
| Get the penalty weight value for the objective function. More... | |
| bool | GetRefGeom (void) const |
| Decide whether it's necessary to read a reference geometry. More... | |
| bool | GetRefGeomSurf (void) const |
| Consider only the surface of the reference geometry. More... | |
| string | GetRefGeom_FEMFileName (void) const |
| Get the name of the file with the reference geometry of the structural problem. More... | |
| unsigned short | GetRefGeom_FileFormat (void) const |
| Get the format of the reference geometry file. More... | |
| STRUCT_2DFORM | GetElas2D_Formulation () const |
| Formulation for 2D elasticity (plane stress - strain) More... | |
| bool | GetPrestretch (void) const |
| Decide whether it's necessary to read a reference geometry. More... | |
| string | GetFEA_FileName (void) const |
| Get the name of the file with the element properties for structural problems. More... | |
| bool | GetAdvanced_FEAElementBased (void) const |
| Determine if advanced features are used from the element-based FEA analysis (experimental feature). More... | |
| string | GetPrestretch_FEMFileName (void) const |
| Get the name of the file with the reference geometry of the structural problem. More... | |
| su2double | GetPoissonRatio (unsigned short id_val) const |
| Get the Poisson's ratio. More... | |
| su2double | GetMaterialDensity (unsigned short id_val) const |
| Get the Material Density. More... | |
| STRUCT_COMPRESS | GetMaterialCompressibility (void) const |
| Compressibility/incompressibility of the solids analysed using the structural solver. More... | |
| STRUCT_MODEL | GetMaterialModel (void) const |
| Compressibility/incompressibility of the solids analysed using the structural solver. More... | |
| STRUCT_DEFORMATION | GetGeometricConditions (void) const |
| Geometric conditions for the structural solver. More... | |
| su2double | GetRefLength (void) const |
| Get the reference length for computing moment (the default value is 1). More... | |
| su2double | GetRefElemLength (void) const |
| Get the reference element length for computing the slope limiting epsilon. More... | |
| su2double | GetRefSharpEdges (void) const |
| Get the reference coefficient for detecting sharp edges. More... | |
| su2double | GetDomainVolume (void) const |
| Get the volume of the whole domain using the fine grid, this value is common for all the grids in the multigrid method. More... | |
| void | SetRefArea (su2double val_area) |
| In case the RefArea is equal to 0 then, it is necessary to compute a reference area, with this function we set the value of the reference area. More... | |
| void | SetSemiSpan (su2double val_semispan) |
| In case the SemiSpan is equal to 0 then, it is necessary to compute the max y distance, with this function we set the value of the semi span. More... | |
| void | SetDomainVolume (su2double val_volume) |
| Set the value of the domain volume computed on the finest grid. More... | |
| void | SetFinestMesh (unsigned short val_finestmesh) |
| Set the finest mesh in a multigrid strategy. More... | |
| void | SetKind_TimeIntScheme (unsigned short val_kind_timeintscheme) |
| Set the kind of time integration scheme. More... | |
| void | SetKind_ConvNumScheme (unsigned short val_kind_convnumscheme, CENTERED val_kind_centered, UPWIND val_kind_upwind, LIMITER val_kind_slopelimit, bool val_muscl, unsigned short val_kind_fem) |
| Set the parameters of the convective numerical scheme. More... | |
| su2double | GetVenkat_LimiterCoeff (void) const |
| Get the value of limiter coefficient. More... | |
| unsigned long | GetLimiterIter (void) const |
| Freeze the value of the limiter after a number of iterations. More... | |
| su2double | GetAdjSharp_LimiterCoeff (void) const |
| Get the value of sharp edge limiter. More... | |
| su2double | GetReynolds (void) const |
| Get the Reynolds number. Dimensionless number that gives a measure of the ratio of inertial forces to viscous forces and consequently quantifies the relative importance of these two types of forces for given flow condition. More... | |
| su2double | GetFroude (void) const |
| Get the Froude number for free surface problems. More... | |
| void | SetFroude (su2double val_froude) |
| Set the Froude number for free surface problems. More... | |
| void | SetMach (su2double val_mach) |
| Set the Mach number. More... | |
| void | SetReynolds (su2double val_reynolds) |
| Set the Reynolds number. More... | |
| void | SetLength_Ref (su2double val_length_ref) |
| Set the reference length for nondimensionalization. More... | |
| void | SetVelocity_Ref (su2double val_velocity_ref) |
| Set the reference velocity for nondimensionalization. More... | |
| void | SetPressure_Ref (su2double val_pressure_ref) |
| Set the reference pressure for nondimensionalization. More... | |
| void | SetDensity_Ref (su2double val_density_ref) |
| Set the reference pressure for nondimensionalization. More... | |
| void | SetTemperature_Ref (su2double val_temperature_ref) |
| Set the reference temperature for nondimensionalization. More... | |
| void | SetTemperature_ve_Ref (su2double val_temperature_ve_ref) |
| Set the reference temperature. More... | |
| void | SetTime_Ref (su2double val_time_ref) |
| Set the reference time for nondimensionalization. More... | |
| void | SetEnergy_Ref (su2double val_energy_ref) |
| Set the reference energy for nondimensionalization. More... | |
| void | SetOmega_Ref (su2double val_omega_ref) |
| Set the reference Omega for nondimensionalization. More... | |
| void | SetForce_Ref (su2double val_force_ref) |
| Set the reference Force for nondimensionalization. More... | |
| void | SetGas_Constant_Ref (su2double val_gas_constant_ref) |
| Set the reference gas-constant for nondimensionalization. More... | |
| void | SetGas_Constant (su2double val_gas_constant) |
| Set the gas-constant. More... | |
| void | SetHeat_Flux_Ref (su2double val_heat_flux_ref) |
| Set the heat flux reference value. More... | |
| void | SetViscosity_Ref (su2double val_viscosity_ref) |
| Set the reference viscosity for nondimensionalization. More... | |
| void | SetConductivity_Ref (su2double val_conductivity_ref) |
| Set the reference conductivity for nondimensionalization. More... | |
| void | SetPressure_FreeStreamND (su2double val_pressure_freestreamnd) |
| Set the nondimensionalized freestream pressure. More... | |
| void | SetPressure_FreeStream (su2double val_pressure_freestream) |
| Set the freestream pressure. More... | |
| void | SetPressure_ThermodynamicND (su2double val_pressure_thermodynamicnd) |
| Set the non-dimensionalized thermodynamic pressure for low Mach problems. More... | |
| void | SetPressure_Thermodynamic (su2double val_pressure_thermodynamic) |
| Set the thermodynamic pressure for low Mach problems. More... | |
| void | SetDensity_FreeStreamND (su2double val_density_freestreamnd) |
| Set the nondimensionalized freestream density. More... | |
| void | SetDensity_FreeStream (su2double val_density_freestream) |
| Set the freestream density. More... | |
| void | SetViscosity_FreeStream (su2double val_viscosity_freestream) |
| Set the freestream viscosity. More... | |
| void | SetModVel_FreeStream (su2double val_modvel_freestream) |
| Set the magnitude of the free-stream velocity. More... | |
| void | SetModVel_FreeStreamND (su2double val_modvel_freestreamnd) |
| Set the non-dimensional magnitude of the free-stream velocity. More... | |
| void | SetTemperature_FreeStream (su2double val_temperature_freestream) |
| Set the freestream temperature. More... | |
| void | SetTemperature_FreeStreamND (su2double val_temperature_freestreamnd) |
| Set the non-dimensional freestream temperature. More... | |
| void | SetTemperature_ve_FreeStream (su2double val_temperature_ve_freestream) |
| Set the freestream vibrational-electronic temperature. More... | |
| void | SetTemperature_ve_FreeStreamND (su2double val_temperature_ve_freestreamnd) |
| Set the non-dimensional freestream vibrational-electronic temperature. More... | |
| void | SetGas_ConstantND (su2double val_gas_constantnd) |
| Set the non-dimensional gas-constant. More... | |
| void | SetVelocity_FreeStream (su2double val_velocity_freestream, unsigned short val_dim) |
| Set the free-stream velocity. More... | |
| void | SetVelocity_FreeStreamND (su2double val_velocity_freestreamnd, unsigned short val_dim) |
| Set the non-dimensional free-stream velocity. More... | |
| void | SetViscosity_FreeStreamND (su2double val_viscosity_freestreamnd) |
| Set the non-dimensional free-stream viscosity. More... | |
| void | SetTke_FreeStreamND (su2double val_tke_freestreamnd) |
| Set the non-dimensional freestream turbulent kinetic energy. More... | |
| void | SetOmega_FreeStreamND (su2double val_omega_freestreamnd) |
| Set the non-dimensional freestream specific dissipation rate omega. More... | |
| void | SetTke_FreeStream (su2double val_tke_freestream) |
| Set the freestream turbulent kinetic energy. More... | |
| void | SetOmega_FreeStream (su2double val_omega_freestream) |
| Set the freestream specific dissipation rate omega. More... | |
| void | SetReThetaT_FreeStream (su2double val_ReThetaT_freestream) |
| Set the freestream momentum thickness Reynolds number. More... | |
| void | SetEnergy_FreeStreamND (su2double val_energy_freestreamnd) |
| Set the non-dimensional freestream energy. More... | |
| void | SetEnergy_FreeStream (su2double val_energy_freestream) |
| Set the freestream energy. More... | |
| void | SetThermalDiffusivity (su2double val_thermal_diffusivity) |
| Set the thermal diffusivity for solids. More... | |
| void | SetTotal_UnstTimeND (su2double val_total_unsttimend) |
| Set the non-dimensional total time for unsteady simulations. More... | |
| su2double | GetAoA (void) const |
| Get the angle of attack of the body. This is the angle between a reference line on a lifting body (often the chord line of an airfoil) and the vector representing the relative motion between the lifting body and the fluid through which it is moving. More... | |
| su2double | GetAoA_Offset (void) const |
| Get the off set angle of attack of the body. The solution and the geometry file are able to modifity the angle of attack in the config file. More... | |
| su2double | GetAoS_Offset (void) const |
| Get the off set sideslip angle of the body. The solution and the geometry file are able to modifity the angle of attack in the config file. More... | |
| su2double | GetAoA_Sens (void) const |
| Get the functional sensitivity with respect to changes in the angle of attack. More... | |
| void | SetAoA (su2double val_AoA) |
| Set the angle of attack. More... | |
| void | SetAoA_Offset (su2double val_AoA_offset) |
| Set the off set angle of attack. More... | |
| void | SetAoS_Offset (su2double val_AoS_offset) |
| Set the off set sideslip angle. More... | |
| void | SetAoA_Sens (su2double val_AoA_sens) |
| Set the angle of attack. More... | |
| void | SetAoS (su2double val_AoS) |
| Set the angle of attack. More... | |
| su2double | GetAoS (void) const |
| Get the angle of sideslip of the body. It relates to the rotation of the aircraft centerline from the relative wind. More... | |
| su2double | GetChargeCoeff (void) const |
| Get the charge coefficient that is used in the poissonal potential simulation. More... | |
| unsigned short | GetnMGLevels (void) const |
| Get the number of multigrid levels. More... | |
| void | SetMGLevels (unsigned short val_nMGLevels) |
| Set the number of multigrid levels. More... | |
| unsigned short | GetFinestMesh (void) const |
| Get the index of the finest grid. More... | |
| unsigned short | GetMGCycle (void) const |
| Get the kind of multigrid (V or W). More... | |
| unsigned short | GetGeometryMode (void) const |
| Get the king of evaluation in the geometrical module. More... | |
| su2double | GetCFL (unsigned short val_mesh) const |
| Get the Courant Friedrich Levi number for each grid. More... | |
| void | SetCFL (unsigned short val_mesh, su2double val_cfl) |
| Get the Courant Friedrich Levi number for each grid. More... | |
| su2double | GetUnst_CFL (void) const |
| Get the Courant Friedrich Levi number for unsteady simulations. More... | |
| bool | GetReorientElements (void) const |
| Get information about element reorientation. More... | |
| su2double | GetMax_DeltaTime (void) const |
| Get the Courant Friedrich Levi number for unsteady simulations. More... | |
| su2double | GetParamDV (unsigned short val_dv, unsigned short val_param) const |
| Get a parameter of the particular design variable. More... | |
| su2double | GetCoordFFDBox (unsigned short val_ffd, unsigned short val_index) const |
| Get the coordinates of the FFD corner points. More... | |
| unsigned short | GetDegreeFFDBox (unsigned short val_ffd, unsigned short val_index) const |
| Get the degree of the FFD corner points. More... | |
| string | GetFFDTag (unsigned short val_dv) const |
| Get the FFD Tag of a particular design variable. More... | |
| string | GetTagFFDBox (unsigned short val_ffd) const |
| Get the FFD Tag of a particular FFD box. More... | |
| unsigned short | GetnDV (void) const |
| Get the number of design variables. More... | |
| unsigned short | GetnDV_Value (unsigned short iDV) const |
| Get the number of design variables. More... | |
| unsigned short | GetnDV_Total (void) const |
| Get the total number of design variables. More... | |
| unsigned short | GetnFFDBox (void) const |
| Get the number of FFD boxes. More... | |
| unsigned short | GetFFD_Continuity (void) const |
| Get the required continuity level at the surface intersection with the FFD. More... | |
| unsigned short | GetFFD_CoordSystem (void) const |
| Get the coordinate system that we are going to use to define the FFD. More... | |
| unsigned short | GetFFD_Blending (void) const |
| Get the kind of FFD Blending function. More... | |
| const su2double * | GetFFD_BSplineOrder () const |
| Get the kind BSpline Order in i,j,k direction. More... | |
| unsigned short | GetnRKStep (void) const |
| Get the number of Runge-Kutta steps. More... | |
| unsigned short | GetnLevels_TimeAccurateLTS (void) const |
| Get the number of time levels for time accurate local time stepping. More... | |
| void | SetnLevels_TimeAccurateLTS (unsigned short val_nLevels) |
| Set the number of time levels for time accurate local time stepping. More... | |
| unsigned short | GetnTimeDOFsADER_DG (void) const |
| Get the number time DOFs for ADER-DG. More... | |
| const su2double * | GetTimeDOFsADER_DG (void) const |
| Get the location of the time DOFs for ADER-DG on the interval [-1..1]. More... | |
| unsigned short | GetnTimeIntegrationADER_DG (void) const |
| Get the number time integration points for ADER-DG. More... | |
| const su2double * | GetTimeIntegrationADER_DG (void) const |
| Get the location of the time integration points for ADER-DG on the interval [-1..1]. More... | |
| const su2double * | GetWeightsIntegrationADER_DG (void) const |
| Get the weights of the time integration points for ADER-DG. More... | |
| unsigned short | GetnMarker_All (void) const |
| Get the total number of boundary markers of the local process including send/receive domains. More... | |
| unsigned short | GetnMarker_CfgFile (void) const |
| Get the total number of boundary markers in the config file. More... | |
| unsigned short | GetnMarker_Euler (void) const |
| Get the number of Euler boundary markers. More... | |
| unsigned short | GetnMarker_SymWall (void) const |
| Get the number of symmetry boundary markers. More... | |
| unsigned short | GetnMarker_Max (void) const |
| Get the total number of boundary markers in the cfg plus the possible send/receive domains. More... | |
| unsigned short | GetnMarker_EngineInflow (void) const |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_EngineExhaust (void) const |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_NearFieldBound (void) const |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_Deform_Mesh (void) const |
| Get the total number of deformable markers at the boundary. More... | |
| unsigned short | GetnMarker_Fluid_Load (void) const |
| Get the total number of markers in which the flow load is computed/employed. More... | |
| unsigned short | GetnMarker_Fluid_InterfaceBound (void) const |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_ActDiskInlet (void) const |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_ActDiskOutlet (void) const |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_Outlet (void) const |
| Get the total number of boundary markers. More... | |
| unsigned short | GetnMarker_Monitoring (void) const |
| Get the total number of monitoring markers. More... | |
| unsigned short | GetnMarker_DV (void) const |
| Get the total number of DV markers. More... | |
| unsigned short | GetnMarker_Moving (void) const |
| Get the total number of moving markers. More... | |
| unsigned short | GetnMarker_SobolevBC (void) const |
| Get the total number of markers for gradient treatment. More... | |
| unsigned short | GetnMarker_PyCustom (void) const |
| Get the total number of Python customizable markers. More... | |
| unsigned short | GetnMarker_Analyze (void) const |
| Get the total number of moving markers. More... | |
| unsigned short | GetnMarker_Periodic (void) const |
| Get the total number of periodic markers. More... | |
| unsigned short | GetnMarker_HeatFlux (void) const |
| Get the total (local) number of heat flux markers. More... | |
| unsigned short | GetnRoughWall (void) const |
| Get the total number of rough markers. More... | |
| unsigned short | GetnObj (void) const |
| Get the total number of objectives in kind_objective list. More... | |
| void | SetnMarker_All (unsigned short val_nmarker) |
| Stores the number of marker in the simulation. More... | |
| long | GetUnst_AdjointIter (void) const |
| Get the starting direct iteration number for the unsteady adjoint (reverse time integration). More... | |
| unsigned long | GetIter_Avg_Objective (void) const |
| Number of iterations to average (reverse time integration). More... | |
| unsigned short | GetnTimeInstances (void) const |
| Retrieves the number of periodic time instances for Harmonic Balance. More... | |
| su2double | GetHarmonicBalance_Period (void) const |
| Retrieves the period of oscillations to be used with Harmonic Balance. More... | |
| void | SetExtIter_OffSet (unsigned long val_iter) |
| Set the current external iteration number. More... | |
| void | SetOuterIter (unsigned long val_iter) |
| Set the current FSI iteration number. More... | |
| void | SetInnerIter (unsigned long val_iter) |
| Set the current FSI iteration number. More... | |
| void | SetTimeIter (unsigned long val_iter) |
| Set the current time iteration number. More... | |
| unsigned long | GetTimeIter () const |
| Get the current time iteration number. More... | |
| unsigned long | GetExtIter_OffSet (void) const |
| Get the current internal iteration number. More... | |
| unsigned long | GetOuterIter (void) const |
| Get the current FSI iteration number. More... | |
| unsigned long | GetInnerIter (void) const |
| Get the current FSI iteration number. More... | |
| void | SetPhysicalTime (su2double val_t) |
| Set the current physical time. More... | |
| su2double | GetPhysicalTime (void) const |
| Get the current physical time. More... | |
| bool | GetWrt_Performance (void) const |
| Get information about writing the performance summary at the end of a calculation. More... | |
| bool | GetWrt_AD_Statistics (void) const |
| Get information about the computational graph (e.g. memory usage) when using AD in reverse mode. More... | |
| bool | GetWrt_MeshQuality (void) const |
| Get information about writing the mesh quality metrics to the visualization files. More... | |
| bool | GetWrt_MultiGrid (void) const |
| Write coarse grids to the visualization files. More... | |
| bool | GetWrt_Projected_Sensitivity (void) const |
| Get information about writing projected sensitivities on surfaces to an ASCII file with rows as x, y, z, dJ/dx, dJ/dy, dJ/dz for each vertex. More... | |
| unsigned short | GetSensitivity_Format (void) const |
| Get information about the format for the input volume sensitvities. More... | |
| bool | GetPlot_Section_Forces (void) const |
| Get information about writing sectional force files. More... | |
| su2double | Get_Alpha_RKStep (unsigned short val_step) const |
| Get the alpha (convective) coefficients for the Runge-Kutta integration scheme. More... | |
| string | GetMarker_All_TagBound (unsigned short val_marker) const |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_ActDiskInlet_TagBound (unsigned short val_marker) const |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_ActDiskOutlet_TagBound (unsigned short val_marker) const |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_Outlet_TagBound (unsigned short val_marker) const |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_EngineInflow_TagBound (unsigned short val_marker) const |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_EngineExhaust_TagBound (unsigned short val_marker) const |
| Get the index of the surface defined in the geometry file. More... | |
| string | GetMarker_Monitoring_TagBound (unsigned short val_marker) const |
| Get the name of the surface defined in the geometry file. More... | |
| string | GetMarker_HeatFlux_TagBound (unsigned short val_marker) const |
| Get the name of the surface defined in the geometry file. More... | |
| short | GetMarker_All_TagBound (string val_tag) |
| Get the tag if the iMarker defined in the geometry file. More... | |
| unsigned short | GetMarker_All_KindBC (unsigned short val_marker) const |
| Get the kind of boundary for each marker. More... | |
| void | SetMarker_All_KindBC (unsigned short val_marker, unsigned short val_boundary) |
| Set the value of the boundary val_boundary (read from the config file) for the marker val_marker. More... | |
| void | SetMarker_All_TagBound (unsigned short val_marker, string val_index) |
| Set the value of the index val_index (read from the geometry file) for the marker val_marker. More... | |
| void | SetMarker_All_Monitoring (unsigned short val_marker, unsigned short val_monitoring) |
| Set if a marker val_marker is going to be monitored val_monitoring (read from the config file). More... | |
| void | SetMarker_All_GeoEval (unsigned short val_marker, unsigned short val_geoeval) |
| Set if a marker val_marker is going to be monitored val_monitoring (read from the config file). More... | |
| void | SetMarker_All_Designing (unsigned short val_marker, unsigned short val_designing) |
| Set if a marker val_marker is going to be designed val_designing (read from the config file). More... | |
| void | SetMarker_All_Plotting (unsigned short val_marker, unsigned short val_plotting) |
| Set if a marker val_marker is going to be plot val_plotting (read from the config file). More... | |
| void | SetMarker_All_Analyze (unsigned short val_marker, unsigned short val_analyze) |
| Set if a marker val_marker is going to be plot val_plotting (read from the config file). More... | |
| void | SetMarker_All_ZoneInterface (unsigned short val_marker, unsigned short val_fsiinterface) |
| Set if a marker val_marker is part of the FSI interface val_plotting (read from the config file). More... | |
| void | SetMarker_All_Turbomachinery (unsigned short val_marker, unsigned short val_turbo) |
| Set if a marker val_marker is part of the Turbomachinery (read from the config file). More... | |
| void | SetMarker_All_TurbomachineryFlag (unsigned short val_marker, unsigned short val_turboflag) |
| Set a flag to the marker val_marker part of the Turbomachinery (read from the config file). More... | |
| void | SetMarker_All_MixingPlaneInterface (unsigned short val_marker, unsigned short val_mixpla_interface) |
| Set if a marker val_marker is part of the MixingPlane interface (read from the config file). More... | |
| void | SetMarker_All_Giles (unsigned short val_marker, unsigned short val_giles) |
| Set if a marker val_marker is part of the Giles boundary (read from the config file). More... | |
| void | SetMarker_All_DV (unsigned short val_marker, unsigned short val_DV) |
| Set if a marker val_marker is going to be affected by design variables val_moving (read from the config file). More... | |
| void | SetMarker_All_Moving (unsigned short val_marker, unsigned short val_moving) |
| Set if a marker val_marker is going to be moved val_moving (read from the config file). More... | |
| void | SetMarker_All_SobolevBC (unsigned short val_marker, unsigned short val_sobolev) |
| Set if a marker how val_marker is going to be applied in gradient treatment. More... | |
| void | SetMarker_All_Deform_Mesh (unsigned short val_marker, unsigned short val_deform) |
| Set if a marker val_marker allows deformation at the boundary. More... | |
| void | SetMarker_All_Deform_Mesh_Sym_Plane (unsigned short val_marker, unsigned short val_deform) |
| Set if a marker val_marker allows deformation at the boundary. More... | |
| void | SetMarker_All_Fluid_Load (unsigned short val_marker, unsigned short val_interface) |
| Set if a in marker val_marker the flow load will be computed/employed. More... | |
| void | SetMarker_All_PyCustom (unsigned short val_marker, unsigned short val_PyCustom) |
| Set if a marker val_marker is going to be customized in Python val_PyCustom (read from the config file). More... | |
| void | SetMarker_All_PerBound (unsigned short val_marker, short val_perbound) |
| Set if a marker val_marker is going to be periodic val_perbound (read from the config file). More... | |
| void | SetMarker_All_SendRecv (unsigned short val_marker, short val_index) |
| Set if a marker val_marker is going to be sent or receive val_index from another domain. More... | |
| short | GetMarker_All_SendRecv (unsigned short val_marker) const |
| Get the send-receive information for a marker val_marker. More... | |
| short | GetMarker_All_PerBound (unsigned short val_marker) const |
| Get an internal index that identify the periodic boundary conditions. More... | |
| unsigned short | GetMarker_All_Monitoring (unsigned short val_marker) const |
| Get the monitoring information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_GeoEval (unsigned short val_marker) const |
| Get the monitoring information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Designing (unsigned short val_marker) const |
| Get the design information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Plotting (unsigned short val_marker) const |
| Get the plotting information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Analyze (unsigned short val_marker) const |
| Get the plotting information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_ZoneInterface (unsigned short val_marker) const |
| Get the FSI interface information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_MixingPlaneInterface (unsigned short val_marker) const |
| Get the MixingPlane interface information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Turbomachinery (unsigned short val_marker) const |
| Get the Turbomachinery information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_TurbomachineryFlag (unsigned short val_marker) const |
| Get the Turbomachinery flag information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Giles (unsigned short val_marker) const |
| Get the Giles boundary information for a marker val_marker. More... | |
| unsigned short | GetMarker_n_ZoneInterface (void) const |
| Get the number of FSI interface markers val_marker. More... | |
| su2double | GetContactResistance (unsigned short val_interface) const |
| Get the contact resistance value of a specified interface. More... | |
| unsigned short | GetMarker_All_DV (unsigned short val_marker) const |
| Get the DV information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_Moving (unsigned short val_marker) const |
| Get the motion information for a marker val_marker. More... | |
| unsigned short | GetMarker_All_SobolevBC (unsigned short val_marker) const |
| Get the information if gradient treatment uses a marker val_marker. More... | |
| unsigned short | GetMarker_All_Deform_Mesh (unsigned short val_marker) const |
| Get whether marker val_marker is a DEFORM_MESH marker. More... | |
| unsigned short | GetMarker_All_Deform_Mesh_Sym_Plane (unsigned short val_marker) const |
| Get whether marker val_marker is a DEFORM_MESH_SYM_PLANE marker. More... | |
| unsigned short | GetMarker_All_Fluid_Load (unsigned short val_marker) const |
| Get whether marker val_marker is a Fluid_Load marker. More... | |
| unsigned short | GetMarker_All_PyCustom (unsigned short val_marker) const |
| Get the Python customization for a marker val_marker. More... | |
| su2double | GetLocationStations (unsigned short val_section) const |
| Get the airfoil sections in the slicing process. More... | |
| su2double | GetNacelleLocation (unsigned short val_index) const |
| Get the defintion of the nacelle location. More... | |
| unsigned short | GetMG_PreSmooth (unsigned short val_mesh) const |
| Get the number of pre-smoothings in a multigrid strategy. More... | |
| unsigned short | GetMG_PostSmooth (unsigned short val_mesh) const |
| Get the number of post-smoothings in a multigrid strategy. More... | |
| unsigned short | GetMG_CorrecSmooth (unsigned short val_mesh) const |
| Get the number of implicit Jacobi smoothings of the correction in a multigrid strategy. More... | |
| short | GetFFD_Fix_IDir (unsigned short val_index) const |
| plane of the FFD (I axis) that should be fixed. More... | |
| short | GetFFD_Fix_JDir (unsigned short val_index) const |
| plane of the FFD (J axis) that should be fixed. More... | |
| short | GetFFD_Fix_KDir (unsigned short val_index) const |
| plane of the FFD (K axis) that should be fixed. More... | |
| unsigned short | GetnFFD_Fix_IDir (void) const |
| Get the number of planes to fix in the I direction. More... | |
| unsigned short | GetnFFD_Fix_JDir (void) const |
| Get the number of planes to fix in the J direction. More... | |
| unsigned short | GetnFFD_Fix_KDir (void) const |
| Get the number of planes to fix in the K direction. More... | |
| MAIN_SOLVER | GetKind_Solver (void) const |
| Governing equations of the flow (it can be different from the run time equation). More... | |
| bool | GetFluidProblem (void) const |
| Return true if a fluid solver is in use. More... | |
| bool | GetStructuralProblem (void) const |
| Return true if a structural solver is in use. More... | |
| bool | GetHeatProblem (void) const |
| Return true if a heat solver is in use. More... | |
| bool | GetFEMSolver (void) const |
| Return true if a high order FEM solver is in use. More... | |
| bool | GetNEMOProblem (void) const |
| Return true if a NEMO solver is in use. More... | |
| bool | GetAUSMMethod (void) const |
| Return true if an AUSM method is in use. More... | |
| ENUM_MULTIZONE | GetKind_MZSolver (void) const |
| Kind of Multizone Solver. More... | |
| ENUM_REGIME | GetKind_Regime (void) const |
| Governing equations of the flow (it can be different from the run time equation). More... | |
| unsigned short | GetSystemMeasurements (void) const |
| Governing equations of the flow (it can be different from the run time equation). More... | |
| string | GetGasModel (void) const |
| Gas model that we are using. More... | |
| TRANSCOEFFMODEL | GetKind_TransCoeffModel (void) const |
| Get the transport coefficient model. More... | |
| unsigned short | GetnWall_Catalytic (void) const |
| Get the total number of heat flux markers. More... | |
| string | GetWall_Catalytic_TagBound (unsigned short val_marker) const |
| Get the name of the surface defined in the geometry file. More... | |
| su2double | GetCatalytic_Efficiency (void) const |
| Get wall catalytic efficiency. More... | |
| unsigned short | GetKind_FluidModel (void) const |
| Fluid model that we are using. More... | |
| ENUM_DATADRIVEN_METHOD | GetKind_DataDriven_Method (void) const |
| Datadriven method for EoS evaluation. More... | |
| const string * | GetDataDriven_FileNames (void) const |
| Get name of the input file for the data-driven fluid model interpolation method. More... | |
| unsigned short | GetNDataDriven_Files (void) const |
| Get number of listed look-up table or multi-layer perceptron input files. More... | |
| su2double | GetRelaxation_DataDriven (void) const |
| Get Newton solver relaxation factor for data-driven fluid models. More... | |
| string | GetFluid_Name (void) const |
| Returns the name of the fluid we are using in CoolProp. More... | |
| INC_DENSITYMODEL | GetKind_DensityModel () const |
| Option to define the density model for incompressible flows. More... | |
| bool | GetVariable_Density_Model () const |
| Selection of variable density option for incompressible flows. More... | |
| bool | GetEnergy_Equation (void) const |
| Flag for whether to solve the energy equation for incompressible flows. More... | |
| FREESTREAM_OPTION | GetKind_FreeStreamOption () const |
| free stream option to initialize the solution More... | |
| unsigned short | GetKind_InitOption (void) const |
| free stream option to initialize the solution More... | |
| su2double | GetPressure_Critical (void) const |
| Get the value of the critical pressure. More... | |
| su2double | GetTemperature_Critical (void) const |
| Get the value of the critical temperature. More... | |
| su2double | GetAcentric_Factor (void) const |
| Get the value of the critical pressure. More... | |
| VISCOSITYMODEL | GetKind_ViscosityModel () const |
| Get the value of the viscosity model. More... | |
| MIXINGVISCOSITYMODEL | GetKind_MixingViscosityModel () const |
| Get the value of the mixing model for viscosity. More... | |
| CONDUCTIVITYMODEL | GetKind_ConductivityModel () const |
| Get the value of the thermal conductivity model. More... | |
| CONDUCTIVITYMODEL_TURB | GetKind_ConductivityModel_Turb () const |
| Get the value of the turbulent thermal conductivity model. More... | |
| DIFFUSIVITYMODEL | GetKind_Diffusivity_Model (void) const |
| Get the value of the mass diffusivity model. More... | |
| su2double | GetMu_Constant (unsigned short val_index=0) const |
| Get the value of the constant viscosity. More... | |
| su2double | GetMu_ConstantND (unsigned short val_index=0) const |
| Get the value of the non-dimensional constant viscosity. More... | |
| su2double | GetThermal_Conductivity_Constant (unsigned short val_index=0) const |
| Get the value of the thermal conductivity. More... | |
| su2double | GetThermal_Conductivity_ConstantND (unsigned short val_index=0) const |
| Get the value of the non-dimensional thermal conductivity. More... | |
| su2double | GetDiffusivity_Constant (void) const |
| Get the value of the constant mass diffusivity for scalar transport. More... | |
| su2double | GetDiffusivity_ConstantND (void) const |
| Get the value of the non-dimensional constant mass diffusivity. More... | |
| su2double | GetSchmidt_Number_Laminar (void) const |
| Get the value of the laminar Schmidt number for scalar transport. More... | |
| su2double | GetSchmidt_Number_Turbulent (void) const |
| Get the value of the turbulent Schmidt number for scalar transport. More... | |
| su2double | GetConstant_Lewis_Number (unsigned short val_index=0) const |
| Get the value of the Lewis number for each species. More... | |
| su2double | GetMu_Ref (unsigned short val_index=0) const |
| Get the value of the reference viscosity for Sutherland model. More... | |
| su2double | GetMu_RefND (unsigned short val_index=0) const |
| Get the value of the non-dimensional reference viscosity for Sutherland model. More... | |
| su2double | GetMu_Temperature_Ref (unsigned short val_index=0) const |
| Get the value of the reference temperature for Sutherland model. More... | |
| su2double | GetMu_Temperature_RefND (unsigned short val_index=0) const |
| Get the value of the non-dimensional reference temperature for Sutherland model. More... | |
| su2double | GetMu_S (unsigned short val_index=0) const |
| Get the value of the reference S for Sutherland model. More... | |
| su2double | GetMu_SND (unsigned short val_index=0) const |
| Get the value of the non-dimensional reference S for Sutherland model. More... | |
| unsigned short | GetnPolyCoeffs (void) const |
| Get the number of coefficients in the temperature polynomial models. More... | |
| su2double | GetCp_PolyCoeff (unsigned short val_index) const |
| Get the temperature polynomial coefficient for specific heat Cp. More... | |
| su2double | GetCp_PolyCoeffND (unsigned short val_index) const |
| Get the temperature polynomial coefficient for specific heat Cp. More... | |
| su2double | GetMu_PolyCoeff (unsigned short val_index) const |
| Get the temperature polynomial coefficient for viscosity. More... | |
| su2double | GetMu_PolyCoeffND (unsigned short val_index) const |
| Get the temperature polynomial coefficient for viscosity. More... | |
| const su2double * | GetMu_PolyCoeffND (void) const |
| Get the temperature polynomial coefficients for viscosity. More... | |
| su2double | GetKt_PolyCoeff (unsigned short val_index) const |
| Get the temperature polynomial coefficient for thermal conductivity. More... | |
| su2double | GetKt_PolyCoeffND (unsigned short val_index) const |
| Get the temperature polynomial coefficient for thermal conductivity. More... | |
| const su2double * | GetKt_PolyCoeffND (void) const |
| Get the temperature polynomial coefficients for thermal conductivity. More... | |
| void | SetCp_PolyCoeffND (su2double val_coeff, unsigned short val_index) |
| Set the temperature polynomial coefficient for specific heat Cp. More... | |
| void | SetMu_PolyCoeffND (su2double val_coeff, unsigned short val_index) |
| Set the temperature polynomial coefficient for viscosity. More... | |
| void | SetKt_PolyCoeffND (su2double val_coeff, unsigned short val_index) |
| Set the temperature polynomial coefficient for thermal conductivity. More... | |
| void | SetDiffusivity_ConstantND (su2double diffusivity_const) |
| Set the value of the non-dimensional constant mass diffusivity. More... | |
| unsigned short | GetKind_Gradient_Method (void) const |
| Get the kind of method for computation of spatial gradients used for viscous and source terms. More... | |
| unsigned short | GetKind_Gradient_Method_Recon (void) const |
| Get the kind of method for computation of spatial gradients used for upwind reconstruction. More... | |
| bool | GetReconstructionGradientRequired (void) const |
| Get flag for whether a second gradient calculation is required for upwind reconstruction alone. More... | |
| bool | GetLeastSquaresRequired (void) const |
| Get flag for whether a least-squares gradient method is being applied. More... | |
| unsigned short | GetKind_Linear_Solver (void) const |
| Get the kind of solver for the implicit solver. More... | |
| unsigned short | GetKind_Linear_Solver_Prec (void) const |
| Get the kind of preconditioner for the implicit solver. More... | |
| unsigned short | GetKind_Deform_Linear_Solver (void) const |
| Get the kind of solver for the implicit solver. More... | |
| su2double | GetLinear_Solver_Error (void) const |
| Get min error of the linear solver for the implicit formulation. More... | |
| su2double | GetDeform_Linear_Solver_Error (void) const |
| Get min error of the linear solver for the implicit formulation. More... | |
| unsigned long | GetLinear_Solver_Iter (void) const |
| Get max number of iterations of the linear solver for the implicit formulation. More... | |
| unsigned long | GetDeform_Linear_Solver_Iter (void) const |
| Get max number of iterations of the linear solver for the implicit formulation. More... | |
| unsigned short | GetLinear_Solver_ILU_n (void) const |
| Get the ILU fill-in level for the linear solver. More... | |
| unsigned long | GetLinear_Solver_Restart_Frequency (void) const |
| Get restart frequency of the linear solver for the implicit formulation. More... | |
| su2double | GetLinear_Solver_Smoother_Relaxation (void) const |
| Get the relaxation factor for iterative linear smoothers. More... | |
| su2double | GetRelaxation_Factor_Adjoint (void) const |
| Get the relaxation factor for solution updates of adjoint solvers. More... | |
| su2double | GetRelaxation_Factor_CHT (void) const |
| Get the relaxation coefficient of the CHT coupling. More... | |
| unsigned short | GetnQuasiNewtonSamples (void) const |
| Get the number of samples used in quasi-Newton methods. More... | |
| bool | GetUseVectorization (void) const |
| Get whether to use vectorized numerics (if available). More... | |
| bool | GetNewtonKrylov (void) const |
| Get whether to use a Newton-Krylov method. More... | |
| array< unsigned short, 3 > | GetNewtonKrylovIntParam (void) const |
| Get Newton-Krylov integer parameters. More... | |
| array< su2double, 4 > | GetNewtonKrylovDblParam (void) const |
| Get Newton-Krylov floating-point parameters. More... | |
| su2double | GetRoe_Kappa (void) const |
| Returns the Roe kappa (multipler of the dissipation term). More... | |
| su2double | GetSemiSpan (void) const |
| Get the wing semi span. More... | |
| unsigned short | GetKind_DiscAdj_Linear_Solver (void) const |
| Get the kind of solver for the implicit solver. More... | |
| unsigned short | GetKind_DiscAdj_Linear_Prec (void) const |
| Get the kind of preconditioner for the implicit solver. More... | |
| unsigned short | GetKind_Deform_Linear_Solver_Prec (void) const |
| Get the kind of preconditioner for the implicit solver. More... | |
| su2double | GetEntropyFix_Coeff (void) const |
| Get the entropy fix. More... | |
| su2double | GetCFLRedCoeff_AdjTurb (void) const |
| Get CFL reduction factor for adjoint turbulence model. More... | |
| unsigned long | GetGridDef_Nonlinear_Iter (void) const |
| Get the number of nonlinear increments for mesh deformation. More... | |
| bool | GetDeform_Mesh (void) const |
| Get information about whether the mesh will be deformed using pseudo linear elasticity. More... | |
| bool | GetDeform_Output (void) const |
| Get information about writing grid deformation residuals to the console. More... | |
| su2double | GetDeform_Coeff (void) const |
| Get factor to multiply smallest volume for deform tolerance. More... | |
| su2double | GetDeform_Limit (void) const |
| Get limit for the volumetric deformation. More... | |
| su2double | GetDeform_ElasticityMod (void) const |
| Get Young's modulus for deformation (constant stiffness deformation) More... | |
| su2double | GetDeform_PoissonRatio (void) const |
| Get Poisson's ratio for deformation (constant stiffness deformation) . More... | |
| unsigned short | GetDeform_Stiffness_Type (void) const |
| Get the type of stiffness to impose for FEA mesh deformation. More... | |
| su2double | GetDeform_StiffLayerSize (void) const |
| Get the size of the layer of highest stiffness for wall distance-based mesh stiffness. More... | |
| bool | GetFFD_Symmetry_Plane (void) const |
| Define the FFD box with a symetry plane. More... | |
| SU2_COMPONENT | GetKind_SU2 (void) const |
| Get the kind of SU2 software component. More... | |
| unsigned short | GetRef_NonDim (void) const |
| Get the kind of non-dimensionalization. More... | |
| unsigned short | GetRef_Inc_NonDim (void) const |
| Get the kind of incompressible non-dimensionalization. More... | |
| void | SetKind_SU2 (SU2_COMPONENT val_kind_su2) |
| Set the kind of SU2 software component. More... | |
| unsigned short | GetnTurbVar (void) const |
| Get the number of Turbulence Variables. More... | |
| TURB_MODEL | GetKind_Turb_Model (void) const |
| Get the kind of the turbulence model. More... | |
| TURB_TRANS_MODEL | GetKind_Trans_Model (void) const |
| Get the kind of the transition model. More... | |
| TURB_TRANS_CORRELATION | GetKind_Trans_Correlation (void) const |
| Get the kind of the transition correlations. More... | |
| su2double | GethRoughness (void) const |
| Get RMS roughness for Transtion model from config. More... | |
| SPECIES_MODEL | GetKind_Species_Model (void) const |
| Get the kind of the species model. More... | |
| TURB_SGS_MODEL | GetKind_SGS_Model (void) const |
| Get the kind of the subgrid scale model. More... | |
| unsigned short | GetKind_TimeIntScheme (void) const |
| Get the kind of time integration method. More... | |
| unsigned short | GetKind_ConvNumScheme (void) const |
| Get the kind of convective numerical scheme. More... | |
| CENTERED | GetKind_Centered (void) const |
| Get kind of center scheme for the convective terms. More... | |
| UPWIND | GetKind_Upwind (void) const |
| Get kind of upwind scheme for the convective terms. More... | |
| bool | GetMUSCL (void) const |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_Flow (void) const |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_Heat (void) const |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_Turb (void) const |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_Species (void) const |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_AdjFlow (void) const |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetMUSCL_AdjTurb (void) const |
| Get if the upwind scheme used MUSCL or not. More... | |
| bool | GetUse_Accurate_Jacobians (void) const |
| Get whether to "Use Accurate Jacobians" for AUSM+up(2) and SLAU(2). More... | |
| unsigned short | GetKind_TimeIntScheme_Flow (void) const |
| Get the kind of integration scheme (explicit or implicit) for the flow equations. More... | |
| unsigned short | GetKind_ADER_Predictor (void) const |
| Get the kind of scheme (aliased or non-aliased) to be used in the predictor step of ADER-DG. More... | |
| unsigned short | GetKind_TimeIntScheme_Heat (void) const |
| Get the kind of integration scheme (explicit or implicit) for the flow equations. More... | |
| unsigned short | GetKind_TimeStep_Heat (void) const |
| Get the kind of time stepping for the heat equation. More... | |
| STRUCT_TIME_INT | GetKind_TimeIntScheme_FEA (void) const |
| Get the kind of integration scheme (explicit or implicit) for the flow equations. More... | |
| unsigned short | GetKind_TimeIntScheme_Radiation (void) const |
| Get the kind of integration scheme (explicit or implicit) for the radiation equations. More... | |
| unsigned short | GetKind_TimeIntScheme_Template (void) |
| Get the kind of integration scheme (explicit or implicit) for the template equations. More... | |
| STRUCT_SPACE_ITE | GetKind_SpaceIteScheme_FEA (void) const |
| Get the kind of integration scheme (explicit or implicit) for the flow equations. More... | |
| unsigned short | GetKind_ConvNumScheme_Flow (void) const |
| Get the kind of convective numerical scheme for the flow equations (centered or upwind). More... | |
| unsigned short | GetKind_ConvNumScheme_FEM_Flow (void) const |
| Get the kind of convective numerical scheme for the flow equations (finite element). More... | |
| unsigned short | GetKind_ConvNumScheme_Template (void) const |
| Get the kind of convective numerical scheme for the template equations (centered or upwind). More... | |
| CENTERED | GetKind_Centered_Flow (void) const |
| Get the kind of center convective numerical scheme for the flow equations. More... | |
| unsigned short | GetKind_Centered_Template (void) |
| Get the kind of center convective numerical scheme for the plasma equations. More... | |
| UPWIND | GetKind_Upwind_Flow (void) const |
| Get the kind of upwind convective numerical scheme for the flow equations. More... | |
| unsigned short | GetKind_FEM_Flow (void) const |
| Get the kind of finite element convective numerical scheme for the flow equations. More... | |
| FEM_SHOCK_CAPTURING_DG | GetKind_FEM_DG_Shock (void) const |
| Get the kind of shock capturing method in FEM DG solver. More... | |
| unsigned short | GetKind_Matrix_Coloring (void) const |
| Get the kind of matrix coloring used for the sparse Jacobian computation. More... | |
| LIMITER | GetKind_SlopeLimit (void) const |
| Get the method for limiting the spatial gradients. More... | |
| LIMITER | GetKind_SlopeLimit_Flow (void) const |
| Get the method for limiting the spatial gradients. More... | |
| LIMITER | GetKind_SlopeLimit_Turb (void) const |
| Get the method for limiting the spatial gradients. More... | |
| LIMITER | GetKind_SlopeLimit_Species () const |
| Get the method for limiting the spatial gradients. More... | |
| LIMITER | GetKind_SlopeLimit_AdjTurb (void) const |
| Get the method for limiting the spatial gradients. More... | |
| LIMITER | GetKind_SlopeLimit_AdjFlow (void) const |
| Get the method for limiting the spatial gradients. More... | |
| su2double | GetKappa_1st_Flow (void) const |
| Value of the calibrated constant for the Lax method (center scheme). More... | |
| su2double | GetKappa_2nd_Flow (void) const |
| Value of the calibrated constant for the JST method (center scheme). More... | |
| su2double | GetKappa_4th_Flow (void) const |
| Value of the calibrated constant for the JST method (center scheme). More... | |
| su2double | GetCent_Jac_Fix_Factor (void) const |
| Factor by which to multiply the dissipation contribution to Jacobians of central schemes. More... | |
| su2double | GetCent_Inc_Jac_Fix_Factor (void) const |
| Factor by which to multiply the dissipation contribution to Jacobians of incompressible central schemes. More... | |
| unsigned short | GetKind_TimeIntScheme_AdjFlow (void) const |
| Get the kind of integration scheme (explicit or implicit) for the adjoint flow equations. More... | |
| unsigned short | GetKind_ConvNumScheme_AdjFlow (void) const |
| Get the kind of convective numerical scheme for the adjoint flow equations (centered or upwind). More... | |
| CENTERED | GetKind_Centered_AdjFlow (void) const |
| Get the kind of center convective numerical scheme for the adjoint flow equations. More... | |
| UPWIND | GetKind_Upwind_AdjFlow (void) const |
| Get the kind of upwind convective numerical scheme for the adjoint flow equations. More... | |
| su2double | GetKappa_2nd_AdjFlow (void) const |
| Value of the calibrated constant for the high order method (center scheme). More... | |
| su2double | GetKappa_4th_AdjFlow (void) const |
| Value of the calibrated constant for the high order method (center scheme). More... | |
| su2double | GetKappa_1st_AdjFlow (void) const |
| Value of the calibrated constant for the low order method (center scheme). More... | |
| unsigned short | GetKind_TimeIntScheme_Turb (void) const |
| Get the kind of integration scheme (implicit) for the turbulence equations. More... | |
| unsigned short | GetKind_ConvNumScheme_Turb (void) const |
| Get the kind of convective numerical scheme for the turbulence equations (upwind). More... | |
| CENTERED | GetKind_Centered_Turb (void) const |
| Get the kind of center convective numerical scheme for the turbulence equations. More... | |
| UPWIND | GetKind_Upwind_Turb (void) const |
| Get the kind of upwind convective numerical scheme for the turbulence equations. More... | |
| unsigned short | GetKind_TimeIntScheme_AdjTurb (void) const |
| Get the kind of integration scheme (explicit or implicit) for the adjoint turbulence equations. More... | |
| unsigned short | GetKind_ConvNumScheme_AdjTurb (void) const |
| Get the kind of convective numerical scheme for the adjoint turbulence equations (centered or upwind). More... | |
| unsigned short | GetKind_TimeIntScheme_Species () const |
| Get the kind of integration scheme (implicit) for the Species equations. More... | |
| unsigned short | GetKind_ConvNumScheme_Species () const |
| Get the kind of convective numerical scheme for the Species equations (upwind). More... | |
| CENTERED | GetKind_Centered_Species () const |
| Get the kind of center convective numerical scheme for the Species equations. More... | |
| UPWIND | GetKind_Upwind_Species () const |
| Get the kind of upwind convective numerical scheme for the Species equations. More... | |
| bool | GetBounded_Species () const |
| Returns true if bounded scalar mode is on for species transport. More... | |
| bool | GetBounded_Turb () const |
| Returns true if bounded scalar mode is on for turbulence transport. More... | |
| bool | GetBounded_Scalar () const |
| Returns true if bounded scalar mode is used for any equation. More... | |
| unsigned short | GetKind_ConvNumScheme_Heat (void) const |
| Get the kind of convective numerical scheme for the heat equation. More... | |
| CENTERED | GetKind_Centered_AdjTurb (void) const |
| Get the kind of center convective numerical scheme for the adjoint turbulence equations. More... | |
| UPWIND | GetKind_Upwind_AdjTurb (void) const |
| Get the kind of upwind convective numerical scheme for the adjoint turbulence equations. More... | |
| bool | GetFrozen_Visc_Cont (void) const |
| Provides information about the way in which the turbulence will be treated by the cont. adjoint method. More... | |
| bool | GetFrozen_Visc_Disc (void) const |
| Provides information about the way in which the turbulence will be treated by the disc. adjoint method. More... | |
| bool | GetInconsistent_Disc (void) const |
| Provides information about using an inconsistent (primal/dual) discrete adjoint formulation. More... | |
| bool | GetFrozen_Limiter_Disc (void) const |
| Provides information about the way in which the limiter will be treated by the disc. adjoint method. More... | |
| bool | GetSens_Remove_Sharp (void) const |
| Provides information about if the sharp edges are going to be removed from the sensitivity. More... | |
| INLET_TYPE | GetKind_Inlet (void) const |
| Get the kind of inlet boundary condition treatment (total conditions or mass flow). More... | |
| bool | GetInlet_Profile_From_File (void) const |
| Check if the inlet profile(s) are specified in an input file. More... | |
| string | GetInlet_FileName (void) const |
| Get name of the input file for the specified inlet profile. More... | |
| string | GetActDisk_FileName (void) const |
| Get name of the input file for the specified actuator disk. More... | |
| su2double | GetInlet_Profile_Matching_Tolerance (void) const |
| Get the tolerance used for matching two points on a specified inlet. More... | |
| INLET_TYPE | GetKind_Inc_Inlet (const string &val_marker) const |
| Get the type of incompressible inlet from the list. More... | |
| unsigned short | GetnInc_Inlet (void) const |
| Get the total number of types in Kind_Inc_Inlet list. More... | |
| bool | GetInc_Inlet_UseNormal (void) const |
| Flag for whether the local boundary normal is used as the flow direction for an incompressible pressure inlet. More... | |
| INC_OUTLET_TYPE | GetKind_Inc_Outlet (const string &val_marker) const |
| Get the type of incompressible outlet from the list. More... | |
| su2double | GetInc_Inlet_Damping (void) const |
| Get the damping factor applied to velocity updates at incompressible pressure inlets. More... | |
| su2double | GetInc_Outlet_Damping (void) const |
| Get the damping factor applied to pressure updates at incompressible mass flow outlet. More... | |
| unsigned short | GetKind_AverageProcess (void) const |
| Get the kind of mixing process for averaging quantities at the boundaries. More... | |
| unsigned short | GetKind_PerformanceAverageProcess (void) const |
| Get the kind of mixing process for averaging quantities at the boundaries. More... | |
| void | SetKind_AverageProcess (unsigned short new_AverageProcess) |
| Set the kind of mixing process for averaging quantities at the boundaries. More... | |
| void | SetKind_PerformanceAverageProcess (unsigned short new_AverageProcess) |
| Set the kind of mixing process for averaging quantities at the boundaries. More... | |
| su2double | GetRampRotatingFrame_Coeff (unsigned short iCoeff) const |
| Get coeff for Rotating Frame Ramp. More... | |
| bool | GetRampRotatingFrame (void) const |
| Get Rotating Frame Ramp option. More... | |
| su2double | GetRampOutletPressure_Coeff (unsigned short iCoeff) const |
| Get coeff for Outlet Pressure Ramp. More... | |
| su2double | GetFinalOutletPressure (void) const |
| Get final Outlet Pressure value for the ramp. More... | |
| su2double | GetMonitorOutletPressure (void) const |
| Get final Outlet Pressure value for the ramp. More... | |
| void | SetMonitorOutletPressure (su2double newMonPres) |
| Set Monitor Outlet Pressure value for the ramp. More... | |
| bool | GetRampOutletPressure (void) const |
| Get Outlet Pressure Ramp option. More... | |
| su2double | GetMixedout_Coeff (unsigned short iCoeff) const |
| Get mixedout coefficients. More... | |
| su2double | GetExtraRelFacGiles (unsigned short iCoeff) const |
| Get extra relaxation factor coefficients for the Giels BC. More... | |
| su2double | GetAverageMachLimit (void) const |
| Get mach limit for average massflow-based procedure . More... | |
| unsigned short | GetKind_MixingPlaneInterface (void) const |
| Get the kind of mixing process for averaging quantities at the boundaries. More... | |
| TURBOMACHINERY_TYPE | GetKind_TurboMachinery (unsigned short val_iZone) const |
| Get the kind of turbomachinery architecture. More... | |
| unsigned short | GetKind_SpanWise (void) const |
| Get the kind of turbomachinery architecture. More... | |
| bool | GetBoolMixingPlaneInterface (void) const |
| Verify if there is mixing plane interface specified from config file. More... | |
| bool | GetBoolTurbMixingPlane (void) const |
| Verify if there is mixing plane interface specified from config file. More... | |
| bool | GetSpatialFourier (void) const |
| Verify if there is mixing plane interface specified from config file. More... | |
| unsigned short | GetnMarker_MixingPlaneInterface (void) const |
| number mixing plane interface specified from config file. More... | |
| bool | GetBoolTurbomachinery (void) const |
| Verify if there is Turbomachinery performance option specified from config file. More... | |
| su2double | GetnBlades (unsigned short val_iZone) const |
| number Turbomachinery blades computed using the pitch information. More... | |
| void | SetnBlades (unsigned short val_iZone, su2double nblades) |
| number Turbomachinery blades computed using the pitch information. More... | |
| bool | GetBoolGiles (void) const |
| Verify if there is any Giles Boundary Condition option specified from config file. More... | |
| bool | GetBoolRiemann (void) const |
| Verify if there is any Riemann Boundary Condition option specified from config file. More... | |
| unsigned short | GetnMarker_Turbomachinery (void) const |
| number Turbomachinery performance option specified from config file. More... | |
| unsigned short | GetnMarker_Shroud (void) const |
| Get number of shroud markers. More... | |
| string | GetMarker_Shroud (unsigned short val_marker) const |
| Get the marker shroud. More... | |
| unsigned short | GetnMarker_TurboPerformance (void) const |
| number Turbomachinery performance option specified from config file. More... | |
| unsigned short | Get_nSpanWiseSections_User (void) const |
| number span-wise sections to compute 3D BC and performance for turbomachinery specified by the user. More... | |
| unsigned short | GetnSpanWiseSections (void) const |
| number span-wise sections to compute 3D BC and performance for turbomachinery. More... | |
| void | SetnSpanMaxAllZones (unsigned short val_nSpna_max) |
| set number of maximum span-wise sections among all zones . More... | |
| unsigned short | GetnSpanMaxAllZones (void) const |
| number span-wise sections to compute performance for turbomachinery. More... | |
| void | SetnSpanWiseSections (unsigned short nSpan) |
| set number span-wise sections to compute 3D BC and performance for turbomachinery. More... | |
| unsigned short | GetnSpan_iZones (unsigned short iZone) const |
| get number span-wise sections to compute 3D BC and performance for turbomachinery. More... | |
| void | SetnSpan_iZones (unsigned short nSpan, unsigned short iZone) |
| set number span-wise sections to compute 3D BC and performance for turbomachinery. More... | |
| string | GetMarker_TurboPerf_BoundIn (unsigned short index) const |
| get inlet bounds name for Turbomachinery performance calculation. More... | |
| string | GetMarker_TurboPerf_BoundOut (unsigned short index) const |
| get outlet bounds name for Turbomachinery performance calculation. More... | |
| TURBO_PERF_KIND | GetKind_TurboPerf (unsigned short val_iZone) const |
| get marker kind for Turbomachinery performance calculation. More... | |
| TURBO_INTERFACE_KIND | GetKind_TurboInterface (unsigned short interfaceIndex) const |
| gets interface kind for an interface marker in turbomachinery problem More... | |
| string | GetMarker_PerBound (unsigned short val_marker) const |
| get outlet bounds name for Turbomachinery performance calculation. More... | |
| unsigned short | GetKind_Engine_Inflow (void) const |
| Get the kind of inlet boundary condition treatment (total conditions or mass flow). More... | |
| unsigned short | GetKind_ActDisk (void) const |
| Get the kind of inlet boundary condition treatment (total conditions or mass flow). More... | |
| void | SetKindWall (string val_marker, unsigned short val_kindwall) |
| Set the kind of wall - rough or smooth. More... | |
| unsigned short | GetnLocationStations (void) const |
| Get the number of sections. More... | |
| unsigned short | GetnWingStations (void) const |
| Get the number of sections for computing internal volume. More... | |
| su2double | GetGeo_Waterline_Location (void) const |
| Get the location of the waterline. More... | |
| bool | GetHold_GridFixed (void) const |
| Provides information about the the nodes that are going to be moved on a deformation volumetric grid deformation. More... | |
| unsigned short | GetKind_ObjFunc (unsigned short val_obj=0) const |
| Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More... | |
| su2double | GetWeight_ObjFunc (unsigned short val_obj) const |
| Get the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More... | |
| void | SetWeight_ObjFunc (unsigned short val_obj, su2double val) |
| Set the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc. More... | |
| const string & | GetCustomObjFunc () const |
| Get the user expression for the custom objective function. More... | |
| const string & | GetCustomOutputs () const |
| Get the user expressions for custom outputs. More... | |
| unsigned short | GetKind_SensSmooth (void) const |
| Get the kind of sensitivity smoothing technique. More... | |
| TIME_MARCHING | GetTime_Marching () const |
| Provides information about the time integration, and change the write in the output files information about the iteration. More... | |
| unsigned short | GetnSpecies () const |
| Provides the number of species present in the gas mixture. More... | |
| const su2double * | GetGas_Composition (void) const |
| Provides the gas mass fractions of the flow. More... | |
| const su2double * | GetSupercatalytic_Wall_Composition (void) const |
| Provides the gas mass fractions at the wall for supercat wall. More... | |
| bool | GetRestart (void) const |
| Provides the restart information. More... | |
| bool | GetRead_Binary_Restart (void) const |
| Flag for whether binary SU2 native restart files are read. More... | |
| bool | GetWrt_Restart_Overwrite (void) const |
| Flag for whether restart solution files are overwritten. More... | |
| bool | GetWrt_Surface_Overwrite (void) const |
| Flag for whether visualization files are overwritten. More... | |
| bool | GetWrt_Volume_Overwrite (void) const |
| Flag for whether visualization files are overwritten. More... | |
| unsigned short | GetnVar (void) |
| Provides the number of varaibles. More... | |
| unsigned short | GetnZone (void) const |
| Provides the number of varaibles. More... | |
| unsigned short | GetiZone (void) const |
| Provides the number of varaibles. More... | |
| bool | GetRestart_Flow (void) const |
| For some problems like adjoint or the linearized equations it is necessary to restart the flow solution. More... | |
| bool | GetFrozen (void) const |
| Indicates whether the flow is frozen (chemistry deactivated). More... | |
| bool | GetIonization (void) const |
| Indicates whether electron gas is present in the gas mixture. More... | |
| bool | GetVTTransferResidualLimiting (void) const |
| Indicates whether the VT source residual is limited. More... | |
| bool | GetMonoatomic (void) const |
| Indicates if mixture is monoatomic. More... | |
| bool | GetSupercatalytic_Wall (void) const |
| Indicates whether supercatalytic wall is used. More... | |
| bool | GetEquivArea (void) const |
| Information about computing and plotting the equivalent area distribution. More... | |
| bool | GetInvDesign_Cp (void) const |
| Information about computing and plotting the equivalent area distribution. More... | |
| bool | GetInvDesign_HeatFlux (void) const |
| Information about computing and plotting the equivalent area distribution. More... | |
| string | GetMesh_FileName (void) const |
| Get name of the input grid. More... | |
| string | GetMesh_Out_FileName (void) const |
| Get name of the output grid, this parameter is important for grid adaptation and deformation. More... | |
| string | GetSolution_FileName (void) const |
| Get the name of the file with the solution of the flow problem. More... | |
| string | GetSolution_AdjFileName (void) const |
| Get the name of the file with the solution of the adjoint flow problem with drag objective function. More... | |
| unsigned short | GetMesh_FileFormat (void) const |
| Get the format of the input/output grid. More... | |
| TAB_OUTPUT | GetTabular_FileFormat (void) const |
| Get the format of the output solution. More... | |
| unsigned short | GetOutput_Precision (void) const |
| Get the output precision to be used in <ofstream>.precision(value) for history and SU2_DOT output. More... | |
| unsigned short | GetActDisk_Jump (void) const |
| Get the format of the output solution. More... | |
| string | GetConv_FileName (void) const |
| Get the name of the file with the convergence history of the problem. More... | |
| unsigned long | GetStartWindowIteration (void) const |
| Get the Starting Iteration for the windowing approach in Sensitivity Analysis for period-averaged outputs, which oscillate. More... | |
| WINDOW_FUNCTION | GetKindWindow (void) const |
| Get Index of the window function used as weight in the cost functional. More... | |
| string | GetBreakdown_FileName (void) const |
| Get the name of the file with the forces breakdown of the problem. More... | |
| string | GetVolume_FileName (void) const |
| Get the name of the file with the flow variables. More... | |
| string | GetFilename (string filename, const string &ext, int Iter) const |
| Add any numbers necessary to the filename (iteration number, zone ID ...) More... | |
| string | GetFilename_Iter (const string &filename_iter, unsigned long curInnerIter, unsigned long curOuterIter) const |
| Add steady iteration number to the filename (does not overwrite previous files) More... | |
| string | GetMultizone_FileName (string val_filename, int val_iZone, const string &ext) const |
| Append the zone index to the restart or the solution files. More... | |
| string | GetMultizone_HistoryFileName (string val_filename, int val_iZone, const string &ext) const |
| Append the zone index to the restart or the solution files. More... | |
| string | GetMultiInstance_FileName (string val_filename, int val_iInst, const string &ext) const |
| Append the instance index to the restart or the solution files. More... | |
| string | GetMultiInstance_HistoryFileName (string val_filename, int val_iInst) const |
| Append the instance index to the restart or the solution files. More... | |
| string | GetRestart_FileName (void) const |
| Get the name of the restart file for the flow variables. More... | |
| string | GetRestart_AdjFileName (void) const |
| Get the name of the restart file for the adjoint variables (drag objective function). More... | |
| string | GetAdj_FileName (void) const |
| Get the name of the file with the adjoint variables. More... | |
| string | GetObjFunc_Grad_FileName (void) const |
| Get the name of the file with the gradient of the objective function. More... | |
| string | GetObjFunc_Value_FileName (void) const |
| Get the name of the file with the gradient of the objective function. More... | |
| string | GetSurfCoeff_FileName (void) const |
| Get the name of the file with the surface information for the flow problem. More... | |
| string | GetSurfAdjCoeff_FileName (void) const |
| Get the name of the file with the surface information for the adjoint problem. More... | |
| string | GetSurfSens_FileName (void) const |
| Get the name of the file with the surface sensitivity (discrete adjoint). More... | |
| string | GetVolSens_FileName (void) const |
| Get the name of the file with the volume sensitivity (discrete adjoint). More... | |
| string | GetUnsteady_FileName (string val_filename, int val_iter, const string &ext) const |
| Augment the input filename with the iteration number for an unsteady file. More... | |
| string | GetObjFunc_Extension (string val_filename) const |
| Append the input filename string with the appropriate objective function extension. More... | |
| unsigned short | GetResidual_Func_Flow (void) const |
| Get functional that is going to be used to evaluate the residual flow convergence. More... | |
| unsigned short | GetCauchy_Func_Flow (void) const |
| Get functional that is going to be used to evaluate the flow convergence. More... | |
| unsigned short | GetCauchy_Func_AdjFlow (void) const |
| Get functional that is going to be used to evaluate the adjoint flow convergence. More... | |
| unsigned short | GetCauchy_Elems (void) const |
| Get the number of iterations that are considered in the Cauchy convergence criteria. More... | |
| unsigned long | GetStartConv_Iter (void) const |
| Get the number of iterations that are not considered in the convergence criteria. More... | |
| su2double | GetCauchy_Eps (void) const |
| Get the value of convergence criteria for the Cauchy method in the direct, adjoint or linearized problem. More... | |
| su2double | GetDelta_UnstTimeND (void) const |
| If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More... | |
| su2double | GetTotal_UnstTimeND (void) const |
| If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More... | |
| su2double | GetDelta_UnstTime (void) const |
| If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation. More... | |
| void | SetDelta_UnstTimeND (su2double val_delta_unsttimend) |
| Set the value of the unsteadty time step using the CFL number. More... | |
| su2double | GetTotal_UnstTime (void) const |
| If we are performing an unsteady simulation, this is the value of max physical time for which we run the simulation. More... | |
| su2double | GetCurrent_UnstTime (void) const |
| If we are performing an unsteady simulation, this is the value of current time. More... | |
| bool | GetSubsonicEngine (void) const |
| Divide the rectbles and hexahedron. More... | |
| bool | GetActDisk_DoubleSurface (void) const |
| Actuator disk defined with a double surface. More... | |
| bool | GetEngine_HalfModel (void) const |
| Only halg of the engine is in the compputational grid. More... | |
| bool | GetActDisk_SU2_DEF (void) const |
| Actuator disk defined with a double surface. More... | |
| su2double & | GetDV_Value (unsigned short val_dv, unsigned short val_val=0) |
| Value of the design variable step, we use this value in design problems. More... | |
| const su2double & | GetDV_Value (unsigned short val_dv, unsigned short val_val=0) const |
| void | SetDV_Value (unsigned short val_dv, unsigned short val_ind, su2double val) |
| Set the value of the design variable step, we use this value in design problems. More... | |
| bool | GetGrid_Movement (void) const |
| Get information about the grid movement. More... | |
| bool | GetDynamic_Grid (void) const |
| Get information about dynamic grids. More... | |
| bool | GetVolumetric_Movement (void) const |
| Get information about the volumetric movement. More... | |
| bool | GetSurface_Movement (unsigned short kind_movement) const |
| Get information about deforming markers. More... | |
| void | SetSurface_Movement (unsigned short iMarker, unsigned short kind_movement) |
| Set a surface movement marker. More... | |
| unsigned short | GetKind_GridMovement () const |
| Get the type of dynamic mesh motion. Each zone gets a config file. More... | |
| void | SetKind_GridMovement (unsigned short motion_Type) |
| Set the type of dynamic mesh motion. More... | |
| unsigned short | GetKind_SurfaceMovement (unsigned short iMarkerMoving) const |
| Get the type of surface motion. More... | |
| su2double | GetMach_Motion (void) const |
| Get the mach number based on the mesh velocity and freestream quantities. More... | |
| su2double | GetMotion_Origin (unsigned short iDim) const |
| Get the mesh motion origin. More... | |
| void | SetMotion_Origin (const su2double *val) |
| Set the mesh motion origin. More... | |
| su2double | GetMarkerMotion_Origin (unsigned short iMarkerMoving, unsigned short iDim) const |
| Get the mesh motion origin. More... | |
| void | SetMarkerMotion_Origin (const su2double *val, unsigned short iMarkerMoving) |
| Set the mesh motion origin. More... | |
| su2double | GetTranslation_Rate (unsigned short iDim) const |
| Get the translational velocity of the mesh. More... | |
| void | SetTranslation_Rate (unsigned short iDim, su2double val) |
| Set the translational velocity of the mesh. More... | |
| su2double | GetMarkerTranslationRate (unsigned short iMarkerMoving, unsigned short iDim) const |
| Get the translational velocity of the marker. More... | |
| void | SetMarkerTranslationRate (unsigned short iMarkerMoving, unsigned short iDim, su2double val) |
| Set the translation rate of the marker. More... | |
| su2double | GetRotation_Rate (unsigned short iDim) const |
| Get the rotation rate of the mesh. More... | |
| void | SetRotation_Rate (unsigned short iDim, su2double val) |
| Get the rotation rate of the mesh. More... | |
| su2double | GetMarkerRotationRate (unsigned short iMarkerMoving, unsigned short iDim) const |
| Get the rotation rate of the marker. More... | |
| void | SetMarkerRotationRate (unsigned short iMarkerMoving, unsigned short iDim, su2double val) |
| Set the rotation rate of the marker. More... | |
| su2double | GetPitching_Omega (unsigned short iDim) const |
| Get the pitching rate of the mesh. More... | |
| su2double | GetMarkerPitching_Omega (unsigned short iMarkerMoving, unsigned short iDim) const |
| Get pitching rate of the marker. More... | |
| su2double | GetPitching_Ampl (unsigned short iDim) const |
| Get the pitching amplitude of the mesh. More... | |
| su2double | GetMarkerPitching_Ampl (unsigned short iMarkerMoving, unsigned short iDim) const |
| Get pitching amplitude of the marker. More... | |
| su2double | GetPitching_Phase (unsigned short iDim) const |
| Get the pitching phase of the mesh. More... | |
| su2double | GetMarkerPitching_Phase (unsigned short iMarkerMoving, unsigned short iDim) const |
| Get pitching phase of the marker. More... | |
| su2double | GetPlunging_Omega (unsigned short iDim) const |
| Get the plunging rate of the mesh. More... | |
| su2double | GetMarkerPlunging_Omega (unsigned short iMarkerMoving, unsigned short iDim) const |
| Get plunging rate of the marker. More... | |
| su2double | GetPlunging_Ampl (unsigned short iDim) const |
| Get the plunging amplitude of the mesh. More... | |
| su2double | GetMarkerPlunging_Ampl (unsigned short iMarkerMoving, unsigned short iDim) const |
| Get plunging amplitude of the marker. More... | |
| su2double | GetFinalRotation_Rate_Z () const |
| Get the angular velocity of the mesh about the z-axis. More... | |
| void | SetRotation_Rate_Z (su2double newRotation_Rate_Z) |
| Set the angular velocity of the mesh about the z-axis. More... | |
| const su2double * | GetOmega_HB (void) const |
| Get the Harmonic Balance frequency pointer. More... | |
| bool | GetHB_Precondition (void) const |
| Get if harmonic balance source term is to be preconditioned. More... | |
| unsigned short | GetMoveMotion_Origin (unsigned short val_marker) const |
| Get if we should update the motion origin. More... | |
| su2double | GetminTurkelBeta () const |
| Get the minimum value of Beta for Roe-Turkel preconditioner. More... | |
| su2double | GetmaxTurkelBeta () const |
| Get the minimum value of Beta for Roe-Turkel preconditioner. More... | |
| bool | GetAdiabaticWall (void) |
| Get information about the adibatic wall condition. More... | |
| bool | GetIsothermalWall (void) |
| Get information about the isothermal wall condition. More... | |
| bool | Low_Mach_Preconditioning (void) const |
| Get information about the Low Mach Preconditioning. More... | |
| bool | Low_Mach_Correction (void) const |
| Get information about the Low Mach Correction. More... | |
| bool | GetPoissonSolver (void) const |
| Get information about the poisson solver condition. More... | |
| bool | GetGravityForce (void) const |
| Get information about the gravity force. More... | |
| bool | GetVorticityConfinement (void) const |
| Get information about the Vorticity Confinement. More... | |
| bool | GetBody_Force (void) const |
| Get information about the body force. More... | |
| const su2double * | GetBody_Force_Vector (void) const |
| Get a pointer to the body force vector. More... | |
| ENUM_STREAMWISE_PERIODIC | GetKind_Streamwise_Periodic (void) const |
| Get information about the streamwise periodicity (None, Pressure_Drop, Massflow). More... | |
| bool | GetStreamwise_Periodic_Temperature (void) const |
| Get information about the streamwise periodicity Energy equation handling. More... | |
| su2double | GetStreamwise_Periodic_OutletHeat (void) const |
| Get the value of the artificial periodic outlet heat. More... | |
| su2double | GetStreamwise_Periodic_PressureDrop (void) const |
| Get the value of the pressure delta from which body force vector is computed. More... | |
| void | SetStreamwise_Periodic_PressureDrop (su2double Streamwise_Periodic_PressureDrop_) |
| Set the value of the pressure delta from which body force vector is computed. Necessary for Restart metadata. More... | |
| su2double | GetStreamwise_Periodic_TargetMassFlow (void) const |
| Get the value of the massflow from which body force vector is computed. More... | |
| bool | GetHeatSource (void) const |
| Get information about the volumetric heat source. More... | |
| su2double | GetHeatSource_Val (void) const |
| Get information about the volumetric heat source. More... | |
| su2double | GetHeatSource_Rot_Z (void) const |
| Get the rotation angle of the volumetric heat source in axis Z. More... | |
| void | SetHeatSource_Rot_Z (su2double val_rot) |
| Set the rotation angle of the volumetric heat source in axis Z. More... | |
| const su2double * | GetHeatSource_Center (void) const |
| Get the position of the center of the volumetric heat source. More... | |
| void | SetHeatSource_Center (su2double x_cent, su2double y_cent, su2double z_cent) |
| Set the position of the center of the volumetric heat source. More... | |
| const su2double * | GetHeatSource_Axes (void) const |
| Get the radius of the ellipsoid that introduces a volumetric heat source. More... | |
| bool | GetRotating_Frame (void) const |
| Get information about the rotational frame. More... | |
| bool | GetAxisymmetric (void) const |
| Get information about the axisymmetric frame. More... | |
| unsigned short | GetSmoothNumGrid (void) const |
| Get information about there is a smoothing of the grid coordinates. More... | |
| void | SubtractFinestMesh (void) |
| Subtract one to the index of the finest grid (full multigrid strategy). More... | |
| unsigned short | GetDesign_Variable (unsigned short val_dv) const |
| Obtain the kind of design variable. More... | |
| su2double | GetBuffet_k (void) const |
| Get the buffet sensor sharpness coefficient. More... | |
| su2double | GetBuffet_lambda (void) const |
| Get the buffet sensor offset parameter. More... | |
| unsigned short | GetMarker_CfgFile_TagBound (const string &val_marker) const |
| Get the index in the config information of the marker val_marker. More... | |
| string | GetMarker_CfgFile_TagBound (unsigned short val_marker) const |
| Get the name in the config information of the marker number val_marker. More... | |
| unsigned short | GetMarker_CfgFile_KindBC (const string &val_marker) const |
| Get the boundary information (kind of boundary) in the config information of the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Monitoring (const string &val_marker) const |
| Get the monitoring information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_GeoEval (const string &val_marker) const |
| Get the monitoring information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Designing (const string &val_marker) const |
| Get the monitoring information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Plotting (const string &val_marker) const |
| Get the plotting information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Analyze (const string &val_marker) const |
| Get the plotting information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_ZoneInterface (const string &val_marker) const |
| Get the multi-physics interface information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Turbomachinery (const string &val_marker) const |
| Get the TurboPerformance information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_TurbomachineryFlag (const string &val_marker) const |
| Get the TurboPerformance flag information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_MixingPlaneInterface (const string &val_marker) const |
| Get the MixingPlane interface information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Giles (const string &val_marker) const |
| Get the Giles boundary information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_DV (const string &val_marker) const |
| Get the DV information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Moving (const string &val_marker) const |
| Get the motion information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_SobolevBC (const string &val_marker) const |
| Get the gradient boundary information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Deform_Mesh (const string &val_marker) const |
| Get the DEFORM_MESH information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Deform_Mesh_Sym_Plane (const string &val_marker) const |
| Get the DEFORM_MESH_SYM_PLANE information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_Fluid_Load (const string &val_marker) const |
| Get the Fluid_Load information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_PyCustom (const string &val_marker) const |
| Get the Python customization information from the config definition for the marker val_marker. More... | |
| unsigned short | GetMarker_CfgFile_PerBound (const string &val_marker) const |
| Get the periodic information from the config definition of the marker val_marker. More... | |
| unsigned short | GetMarker_ZoneInterface (const string &val_marker) const |
| Get the name of the marker val_marker. More... | |
| string | GetMarkerTag_ZoneInterface (unsigned short val_iMarker) const |
| Get the name of the marker val_iMarker. More... | |
| unsigned short | GetnMarker_ZoneInterface (void) const |
| Get the number of markers in the multizone interface. More... | |
| bool | GetSolid_Wall (unsigned short iMarker) const |
| Determines whether a marker with index iMarker is a solid boundary. More... | |
| bool | GetViscous_Wall (unsigned short iMarker) const |
| Determines whether a marker with index iMarker is a viscous no-slip boundary. More... | |
| bool | GetCatalytic_Wall (unsigned short iMarker) const |
| Determines whether a marker with index iMarker is a catalytic boundary. More... | |
| bool | GetContinuous_Adjoint (void) const |
| Determines if problem is adjoint. More... | |
| bool | GetViscous (void) const |
| Determines if problem is viscous. More... | |
| bool | GetCatalytic (void) const |
| Determines if problem has catalytic walls. More... | |
| unsigned short | GetContainerPosition (unsigned short val_eqsystem) |
| Provides the index of the solution in the container. More... | |
| su2double | GetMinLogResidual (void) const |
| Value of the minimum residual value (log10 scale). More... | |
| unsigned long | GetBc_Eval_Freq (void) const |
| Evaluation frequency for Engine and Actuator disk markers. More... | |
| su2double | GetDamp_Engine_Inflow (void) const |
| Value of the damping factor for the engine inlet bc. More... | |
| su2double | GetDamp_Engine_Exhaust (void) const |
| Value of the damping factor for the engine exhaust inlet bc. More... | |
| su2double | GetDamp_Res_Restric (void) const |
| Value of the damping factor for the residual restriction. More... | |
| su2double | GetDamp_Correc_Prolong (void) const |
| Value of the damping factor for the correction prolongation. More... | |
| su2double | GetPosition_Plane (void) const |
| Value of the position of the Near Field (y coordinate for 2D, and z coordinate for 3D). More... | |
| su2double | GetWeightCd (void) const |
| Value of the weight of the drag coefficient in the Sonic Boom optimization. More... | |
| void | SetdNetThrust_dBCThrust (su2double val_dnetthrust_dbcthrust) |
| Value of the damping factor for the Thrust BC (actuator disk). More... | |
| su2double | GetFixAzimuthalLine (void) const |
| Value of the azimuthal line to fix due to a misalignments of the nearfield. More... | |
| su2double | GetdCD_dCL (void) const |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCD_dCL (su2double val_dcd_dcl) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetdCMx_dCL (void) const |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCMx_dCL (su2double val_dcmx_dcl) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetdCMy_dCL (void) const |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCMy_dCL (su2double val_dcmy_dcl) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetdCMz_dCL (void) const |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCMz_dCL (su2double val_dcmz_dcl) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetdCL_dAlpha (su2double val_dcl_dalpha) |
| Value of the weight of the CD, CL, CM optimization. More... | |
| su2double | GetCL_Target (void) const |
| Value of the weight of the CD, CL, CM optimization. More... | |
| void | SetGlobalParam (MAIN_SOLVER val_solver, unsigned short val_system) |
| Set the global parameters of each simulation for each runtime system. More... | |
| const su2double * | GetPeriodicRotCenter (const string &val_marker) const |
| Center of rotation for a rotational periodic boundary. More... | |
| const su2double * | GetPeriodicRotAngles (const string &val_marker) const |
| Angles of rotation for a rotational periodic boundary. More... | |
| const su2double * | GetPeriodicTranslation (const string &val_marker) const |
| Translation vector for a translational periodic boundary. More... | |
| const su2double * | GetPeriodic_Translation (unsigned short val_index) const |
| Get the translation vector for a periodic transformation. More... | |
| unsigned short | GetMarker_Periodic_Donor (const string &val_marker) const |
| Get the rotationally periodic donor marker for boundary val_marker. More... | |
| su2double | GetActDisk_NetThrust (const string &val_marker) const |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_Power (const string &val_marker) const |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_MassFlow (const string &val_marker) const |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_Mach (const string &val_marker) const |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_Force (const string &val_marker) const |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_BCThrust (const string &val_marker) const |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_BCThrust_Old (const string &val_marker) const |
| Get the origin of the actuator disk. More... | |
| su2double | GetActDisk_Area (const string &val_marker) const |
| Get the tip radius of th actuator disk. More... | |
| su2double | GetActDisk_ReverseMassFlow (const string &val_marker) const |
| Get the tip radius of th actuator disk. More... | |
| su2double | GetActDisk_PressJump (const string &val_marker, unsigned short val_index) const |
| Get the thrust corffient of the actuator disk. More... | |
| su2double | GetActDisk_TempJump (const string &val_marker, unsigned short val_index) const |
| Get the thrust corffient of the actuator disk. More... | |
| su2double | GetActDisk_Omega (const string &val_marker, unsigned short val_index) const |
| Get the rev / min of the actuator disk. More... | |
| su2double | GetActDiskBem_CG (unsigned short iDim, string val_marker, unsigned short val_index) const |
| Get the Center of the actuator disk with BEM. More... | |
| su2double | GetActDiskBem_Axis (unsigned short iDim, string val_marker, unsigned short val_index) const |
| Get the axis of the actuator disk with BEM. More... | |
| const unsigned short & | GetActDiskBem_Frequency (void) const |
| Get the frequency of updating the actuator disk with BEM. More... | |
| su2double | GetBEM_blade_angle (void) const |
| Get the blade angle of the propeller. More... | |
| const string & | GetBEM_prop_filename (void) const |
| Get the filename of the propeller. More... | |
| unsigned short | GetMarker_CfgFile_ActDiskOutlet (const string &val_marker) const |
| Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet). More... | |
| unsigned short | GetMarker_CfgFile_EngineExhaust (const string &val_marker) const |
| Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet). More... | |
| unsigned short | GetMarker_Moving (const string &val_marker) const |
| Get the internal index for a moving boundary val_marker. More... | |
| bool | GetMarker_Moving_Bool (const string &val_marker) const |
| Get a bool for whether a marker is moving. val_marker. More... | |
| unsigned short | GetMarker_Deform_Mesh (const string &val_marker) const |
| Get the internal index for a DEFORM_MESH boundary val_marker. More... | |
| unsigned short | GetMarker_Deform_Mesh_Sym_Plane (const string &val_marker) const |
| Get the internal index for a DEFORM_MESH_SYM_PLANE boundary val_marker. More... | |
| bool | GetMarker_Deform_Mesh_Bool (const string &val_marker) const |
| Get a bool for whether the marker is deformed. val_marker. More... | |
| unsigned short | GetMarker_Fluid_Load (const string &val_marker) const |
| Get the internal index for a Fluid_Load boundary val_marker. More... | |
| unsigned short | GetMarker_SobolevBC (const string &val_marker) const |
| Get the internal index for a gradient boundary condition val_marker. More... | |
| string | GetMarker_Moving_TagBound (unsigned short val_marker) const |
| Get the name of the surface defined in the geometry file. More... | |
| string | GetMarker_Deform_Mesh_TagBound (unsigned short val_marker) const |
| Get the name of the DEFORM_MESH boundary defined in the geometry file. More... | |
| string | GetMarker_Deform_Mesh_Sym_Plane_TagBound (unsigned short val_marker) const |
| Get the name of the DEFORM_MESH_SYM_PLANE boundary defined in the geometry file. More... | |
| string | GetMarker_Fluid_Load_TagBound (unsigned short val_marker) const |
| Get the name of the Fluid_Load boundary defined in the geometry file. More... | |
| string | GetMarker_PyCustom_TagBound (unsigned short val_marker) const |
| Get the name of the surface defined in the geometry file. More... | |
| string | GetMarker_Analyze_TagBound (unsigned short val_marker) const |
| Get the name of the surface defined in the geometry file. More... | |
| su2double | GetExhaust_Temperature_Target (const string &val_index) const |
| Get the total temperature at a nacelle boundary. More... | |
| su2double | GetInletTtotal (const string &val_index) const |
| Get the total temperature at an inlet boundary. More... | |
| su2double | GetInlet_Temperature (const string &val_index) const |
| Get the temperature at a supersonic inlet boundary. More... | |
| su2double | GetInlet_Pressure (const string &val_index) const |
| Get the pressure at a supersonic inlet boundary. More... | |
| const su2double * | GetInlet_Velocity (const string &val_index) const |
| Get the velocity vector at a supersonic inlet boundary. More... | |
| const su2double * | GetInlet_MassFrac () const |
| Get the mass fraction vector for a NEMO inlet boundary. More... | |
| su2double | GetInlet_Temperature_ve () const |
| Get the Tve value for a NEMO inlet boundary. More... | |
| su2double | GetInletPtotal (const string &val_index) const |
| Get the total pressure at an inlet boundary. More... | |
| void | SetInletPtotal (su2double val_pressure, const string &val_marker) |
| Set the total pressure at an inlet boundary. More... | |
| const su2double * | GetInlet_SpeciesVal (const string &val_index) const |
| Get the species values at an inlet boundary. More... | |
| const su2double * | GetInlet_TurbVal (const string &val_index) const |
| Get the turbulent properties values at an inlet boundary. More... | |
| su2double | GetExhaust_Pressure_Target (const string &val_index) const |
| Get the total pressure at an nacelle boundary. More... | |
| su2double | GetCFLRedCoeff_Turb (void) const |
| Value of the CFL reduction in turbulence problems. More... | |
| su2double | GetCFLRedCoeff_Species () const |
| Value of the CFL reduction in species problems. More... | |
| const su2double * | GetInletFlowDir (const string &val_index) const |
| Get the flow direction unit vector at an inlet boundary. More... | |
| su2double | GetOutlet_Pressure (const string &val_index) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetOutlet_Pressure (su2double val_pressure, const string &val_marker) |
| Set the back pressure (static) at an outlet boundary. More... | |
| su2double | GetRiemann_Var1 (const string &val_marker) const |
| Get the var 1 at Riemann boundary. More... | |
| su2double | GetRiemann_Var2 (const string &val_marker) const |
| Get the var 2 at Riemann boundary. More... | |
| const su2double * | GetRiemann_FlowDir (const string &val_marker) const |
| Get the Flowdir at Riemann boundary. More... | |
| unsigned short | GetKind_Data_Riemann (const string &val_marker) const |
| Get Kind Data of Riemann boundary. More... | |
| su2double | GetGiles_Var1 (const string &val_marker) const |
| Get the var 1 for the Giels BC. More... | |
| su2double | GetGiles_Var2 (const string &val_marker) const |
| Get the var 2 for the Giles boundary. More... | |
| const su2double * | GetGiles_FlowDir (const string &val_marker) const |
| Get the Flowdir for the Giles BC. More... | |
| unsigned short | GetKind_Data_Giles (const string &val_marker) const |
| Get Kind Data for the Giles BC. More... | |
| void | SetGiles_Var1 (su2double newVar1, const string &val_marker) |
| Set the var 1 for Giles BC. More... | |
| su2double | GetGiles_RelaxFactorAverage (const string &val_marker) const |
| Get the relax factor for the average component for the Giles BC. More... | |
| su2double | GetGiles_RelaxFactorFourier (const string &val_marker) const |
| Get the relax factor for the fourier component for the Giles BC. More... | |
| su2double | GetPressureOut_BC () const |
| Get the outlet pressure imposed as BC for internal flow. More... | |
| void | SetPressureOut_BC (su2double val_press) |
| Set the outlet pressure imposed as BC for internal flow. More... | |
| su2double | GetIncInlet_BC () const |
| Get the inlet velocity or pressure imposed for incompressible flow. More... | |
| void | SetIncInlet_BC (su2double val_in) |
| Set the inlet velocity or pressure imposed as BC for incompressible flow. More... | |
| su2double | GetIncTemperature_BC () const |
| Get the inlet temperature imposed as BC for incompressible flow. More... | |
| void | SetIncTemperature_BC (su2double val_temperature) |
| Set the inlet temperature imposed as BC for incompressible flow. More... | |
| su2double | GetIncPressureOut_BC () const |
| Get the outlet pressure imposed as BC for incompressible flow. More... | |
| void | SetIncPressureOut_BC (su2double val_pressure) |
| Set the outlet pressure imposed as BC for incompressible flow. More... | |
| su2double | GetTotalPressureIn_BC () const |
| Get the inlet total pressure imposed as BC for internal flow. More... | |
| su2double | GetTotalTemperatureIn_BC () const |
| Get the inlet total temperature imposed as BC for internal flow. More... | |
| void | SetTotalTemperatureIn_BC (su2double val_temp) |
| Set the inlet total temperature imposed as BC for internal flow. More... | |
| su2double | GetFlowAngleIn_BC () const |
| Get the inlet flow angle imposed as BC for internal flow. More... | |
| su2double | GetIsothermal_Temperature (const string &val_index) const |
| Get the wall temperature (static) at an isothermal boundary. More... | |
| su2double | GetWall_HeatFlux (const string &val_index) const |
| Get the wall heat flux on a constant heat flux boundary. More... | |
| su2double | GetWall_HeatTransfer_Coefficient (const string &val_index) const |
| Get the heat transfer coefficient on a heat transfer boundary. More... | |
| su2double | GetWall_HeatTransfer_Temperature (const string &val_index) const |
| Get the temperature at inifinty on a heat transfer boundary. More... | |
| WALL_FUNCTIONS | GetWallFunction_Treatment (const string &val_marker) const |
| Get the wall function treatment for the given boundary marker. More... | |
| const unsigned short * | GetWallFunction_IntInfo (const string &val_marker) const |
| Get the additional integer info for the wall function treatment for the given boundary marker. More... | |
| const su2double * | GetWallFunction_DoubleInfo (const string &val_marker) const |
| Get the additional double info for the wall function treatment for the given boundary marker. More... | |
| pair< WALL_TYPE, su2double > | GetWallRoughnessProperties (const string &val_marker) const |
| Get the type of wall and roughness height on a wall boundary (Heatflux or Isothermal). More... | |
| su2double | GetEngineInflow_Target (const string &val_marker) const |
| Get the target (pressure, massflow, etc) at an engine inflow boundary. More... | |
| su2double | GetInflow_Mach (const string &val_marker) const |
| Get the fan face Mach number at an engine inflow boundary. More... | |
| su2double | GetInflow_Pressure (const string &val_marker) const |
| Get the back pressure (static) at an engine inflow boundary. More... | |
| su2double | GetInflow_MassFlow (const string &val_marker) const |
| Get the mass flow rate at an engine inflow boundary. More... | |
| su2double | GetInflow_ReverseMassFlow (const string &val_marker) const |
| Get the percentage of reverse flow at an engine inflow boundary. More... | |
| su2double | GetInflow_ReverseMassFlow (unsigned short val_marker) const |
| Get the percentage of reverse flow at an engine inflow boundary. More... | |
| su2double | GetInflow_TotalPressure (const string &val_marker) const |
| Get the total pressure at an engine inflow boundary. More... | |
| su2double | GetInflow_Temperature (const string &val_marker) const |
| Get the temperature (static) at an engine inflow boundary. More... | |
| su2double | GetInflow_TotalTemperature (const string &val_marker) const |
| Get the total temperature at an engine inflow boundary. More... | |
| su2double | GetInflow_RamDrag (const string &val_marker) const |
| Get the ram drag at an engine inflow boundary. More... | |
| su2double | GetInflow_Force (const string &val_marker) const |
| Get the force balance at an engine inflow boundary. More... | |
| su2double | GetInflow_Power (const string &val_marker) const |
| Get the power at an engine inflow boundary. More... | |
| su2double | GetExhaust_Pressure (const string &val_marker) const |
| Get the back pressure (static) at an engine exhaust boundary. More... | |
| su2double | GetExhaust_Temperature (const string &val_marker) const |
| Get the temperature (static) at an engine exhaust boundary. More... | |
| su2double | GetExhaust_MassFlow (const string &val_marker) const |
| Get the massflow at an engine exhaust boundary. More... | |
| su2double | GetExhaust_TotalPressure (const string &val_marker) const |
| Get the total pressure at an engine exhaust boundary. More... | |
| su2double | GetExhaust_TotalTemperature (const string &val_marker) const |
| Get the total temperature at an engine exhaust boundary. More... | |
| su2double | GetExhaust_GrossThrust (const string &val_marker) const |
| Get the gross thrust at an engine exhaust boundary. More... | |
| su2double | GetExhaust_Force (const string &val_marker) const |
| Get the force balance at an engine exhaust boundary. More... | |
| su2double | GetExhaust_Power (const string &val_marker) const |
| Get the power at an engine exhaust boundary. More... | |
| void | SetInflow_Mach (unsigned short val_marker, su2double val_fanface_mach) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetInflow_Pressure (unsigned short val_marker, su2double val_fanface_pressure) |
| Set the fan face static pressure at an engine inflow boundary. More... | |
| void | SetInflow_MassFlow (unsigned short val_marker, su2double val_fanface_massflow) |
| Set the massflow at an engine inflow boundary. More... | |
| void | SetInflow_ReverseMassFlow (unsigned short val_marker, su2double val_fanface_reversemassflow) |
| Set the reverse flow at an engine inflow boundary. More... | |
| void | SetInflow_TotalPressure (unsigned short val_marker, su2double val_fanface_totalpressure) |
| Set the fan face total pressure at an engine inflow boundary. More... | |
| void | SetInflow_Temperature (unsigned short val_marker, su2double val_fanface_temperature) |
| Set the fan face static temperature at an engine inflow boundary. More... | |
| void | SetInflow_TotalTemperature (unsigned short val_marker, su2double val_fanface_totaltemperature) |
| Set the fan face total temperature at an engine inflow boundary. More... | |
| void | SetInflow_RamDrag (unsigned short val_marker, su2double val_fanface_ramdrag) |
| Set the ram drag temperature at an engine inflow boundary. More... | |
| void | SetInflow_Force (unsigned short val_marker, su2double val_fanface_force) |
| Set the force balance at an engine inflow boundary. More... | |
| void | SetInflow_Power (unsigned short val_marker, su2double val_fanface_power) |
| Set the power at an engine inflow boundary. More... | |
| void | SetExhaust_Pressure (unsigned short val_marker, su2double val_exhaust_pressure) |
| Set the back pressure (static) at an engine exhaust boundary. More... | |
| void | SetExhaust_Temperature (unsigned short val_marker, su2double val_exhaust_temp) |
| Set the temperature (static) at an engine exhaust boundary. More... | |
| void | SetExhaust_MassFlow (unsigned short val_marker, su2double val_exhaust_massflow) |
| Set the back pressure (static) at an engine exhaust boundary. More... | |
| void | SetExhaust_TotalPressure (unsigned short val_marker, su2double val_exhaust_totalpressure) |
| Set the back pressure (total) at an engine exhaust boundary. More... | |
| void | SetExhaust_TotalTemperature (unsigned short val_marker, su2double val_exhaust_totaltemp) |
| Set the total temperature at an engine exhaust boundary. More... | |
| void | SetExhaust_GrossThrust (unsigned short val_marker, su2double val_exhaust_grossthrust) |
| Set the gross thrust at an engine exhaust boundary. More... | |
| void | SetExhaust_Force (unsigned short val_marker, su2double val_exhaust_force) |
| Set the force balance at an engine exhaust boundary. More... | |
| void | SetExhaust_Power (unsigned short val_marker, su2double val_exhaust_power) |
| Set the power at an engine exhaust boundary. More... | |
| void | SetEngine_Mach (unsigned short val_marker, su2double val_engine_mach) |
| Set the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_Force (unsigned short val_marker, su2double val_engine_force) |
| Set the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_Power (unsigned short val_marker, su2double val_engine_power) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_NetThrust (unsigned short val_marker, su2double val_engine_netthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_GrossThrust (unsigned short val_marker, su2double val_engine_grossthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetEngine_Area (unsigned short val_marker, su2double val_engine_area) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_Mach (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_Force (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_Power (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_NetThrust (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_GrossThrust (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetEngine_Area (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_Temperature (unsigned short val_marker, su2double val_actdisk_temp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_TotalTemperature (unsigned short val_marker, su2double val_actdisk_totaltemp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_Temperature (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_TotalTemperature (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_Temperature (unsigned short val_marker, su2double val_actdisk_temp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_TotalTemperature (unsigned short val_marker, su2double val_actdisk_totaltemp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_Temperature (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_TotalTemperature (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_MassFlow (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_MassFlow (unsigned short val_marker, su2double val_actdisk_massflow) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_MassFlow (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_MassFlow (unsigned short val_marker, su2double val_actdisk_massflow) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_Pressure (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_TotalPressure (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_DeltaPress (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_DeltaTemp (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_TotalPressRatio (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_TotalTempRatio (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_StaticPressRatio (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_StaticTempRatio (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_NetThrust (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_BCThrust (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_BCThrust_Old (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_GrossThrust (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_Area (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_ReverseMassFlow (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_RamDrag (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_Force (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskInlet_Power (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_Pressure (unsigned short val_marker, su2double val_actdisk_press) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_TotalPressure (unsigned short val_marker, su2double val_actdisk_totalpress) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_DeltaPress (unsigned short val_marker, su2double val_actdisk_deltapress) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_Power (unsigned short val_marker, su2double val_actdisk_power) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_MassFlow (unsigned short val_marker, su2double val_actdisk_massflow) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_Mach (unsigned short val_marker, su2double val_actdisk_mach) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_Force (unsigned short val_marker, su2double val_actdisk_force) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetOutlet_MassFlow (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetOutlet_MassFlow (unsigned short val_marker, su2double val_massflow) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetOutlet_Density (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetOutlet_Density (unsigned short val_marker, su2double val_density) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetOutlet_Area (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetOutlet_Area (unsigned short val_marker, su2double val_area) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetSurface_DC60 (unsigned short val_marker, su2double val_surface_distortion) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetSurface_MassFlow (unsigned short val_marker, su2double val_surface_massflow) |
| Set the massflow at the surface. More... | |
| void | SetSurface_Mach (unsigned short val_marker, su2double val_surface_mach) |
| Set the mach number at the surface. More... | |
| void | SetSurface_Temperature (unsigned short val_marker, su2double val_surface_temperature) |
| Set the temperature at the surface. More... | |
| void | SetSurface_Pressure (unsigned short val_marker, su2double val_surface_pressure) |
| Set the pressure at the surface. More... | |
| void | SetSurface_Density (unsigned short val_marker, su2double val_surface_density) |
| Set the density at the surface. More... | |
| void | SetSurface_Enthalpy (unsigned short val_marker, su2double val_surface_enthalpy) |
| Set the enthalpy at the surface. More... | |
| void | SetSurface_NormalVelocity (unsigned short val_marker, su2double val_surface_normalvelocity) |
| Set the normal velocity at the surface. More... | |
| void | SetSurface_Uniformity (unsigned short val_marker, su2double val_surface_streamwiseuniformity) |
| Set the streamwise flow uniformity at the surface. More... | |
| void | SetSurface_SecondaryStrength (unsigned short val_marker, su2double val_surface_secondarystrength) |
| Set the secondary flow strength at the surface. More... | |
| void | SetSurface_SecondOverUniform (unsigned short val_marker, su2double val_surface_secondaryoverstream) |
| Set the relative secondary flow strength at the surface. More... | |
| void | SetSurface_MomentumDistortion (unsigned short val_marker, su2double val_surface_momentumdistortion) |
| Set the momentum distortion at the surface. More... | |
| void | SetSurface_TotalTemperature (unsigned short val_marker, su2double val_surface_totaltemperature) |
| Set the total temperature at the surface. More... | |
| void | SetSurface_TotalPressure (unsigned short val_marker, su2double val_surface_totalpressure) |
| Set the total pressure at the surface. More... | |
| void | SetSurface_PressureDrop (unsigned short val_marker, su2double val_surface_pressuredrop) |
| Set the pressure drop between two surfaces. More... | |
| void | SetSurface_Species_0 (unsigned short val_marker, su2double val_surface_species_0) |
| Set the average of species_0 at the surface. More... | |
| void | SetSurface_Species_Variance (unsigned short val_marker, su2double val_surface_species_variance) |
| Set the species variance at the surface. More... | |
| void | SetSurface_IDC (unsigned short val_marker, su2double val_surface_distortion) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetSurface_IDC_Mach (unsigned short val_marker, su2double val_surface_distortion) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetSurface_IDR (unsigned short val_marker, su2double val_surface_distortion) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_DeltaTemp (unsigned short val_marker, su2double val_actdisk_deltatemp) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_TotalPressRatio (unsigned short val_marker, su2double val_actdisk_pressratio) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_TotalTempRatio (unsigned short val_marker, su2double val_actdisk_tempratio) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_StaticPressRatio (unsigned short val_marker, su2double val_actdisk_pressratio) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_StaticTempRatio (unsigned short val_marker, su2double val_actdisk_tempratio) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_NetThrust (unsigned short val_marker, su2double val_actdisk_netthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_BCThrust (const string &val_marker, su2double val_actdisk_bcthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_BCThrust (unsigned short val_marker, su2double val_actdisk_bcthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_BCThrust_Old (const string &val_marker, su2double val_actdisk_bcthrust_old) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_BCThrust_Old (unsigned short val_marker, su2double val_actdisk_bcthrust_old) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_GrossThrust (unsigned short val_marker, su2double val_actdisk_grossthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDisk_Area (unsigned short val_marker, su2double val_actdisk_area) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_ReverseMassFlow (unsigned short val_marker, su2double val_actdisk_area) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_RamDrag (unsigned short val_marker, su2double val_actdisk_ramdrag) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_Force (unsigned short val_marker, su2double val_actdisk_force) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskInlet_Power (unsigned short val_marker, su2double val_actdisk_power) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_Power (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_MassFlow (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_Mach (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDisk_Force (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetSurface_DC60 (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetSurface_MassFlow (unsigned short val_marker) const |
| Get the massflow at an outlet boundary. More... | |
| su2double | GetSurface_Mach (unsigned short val_marker) const |
| Get the mach number at an outlet boundary. More... | |
| su2double | GetSurface_Temperature (unsigned short val_marker) const |
| Get the temperature at an outlet boundary. More... | |
| su2double | GetSurface_Pressure (unsigned short val_marker) const |
| Get the pressure at an outlet boundary. More... | |
| su2double | GetSurface_Density (unsigned short val_marker) const |
| Get the density at an outlet boundary. More... | |
| su2double | GetSurface_Enthalpy (unsigned short val_marker) const |
| Get the enthalpy at an outlet boundary. More... | |
| su2double | GetSurface_NormalVelocity (unsigned short val_marker) const |
| Get the normal velocity at an outlet boundary. More... | |
| su2double | GetSurface_Uniformity (unsigned short val_marker) const |
| Get the streamwise flow uniformity at the surface. More... | |
| su2double | GetSurface_SecondaryStrength (unsigned short val_marker) const |
| Get the secondary flow strength at the surface. More... | |
| su2double | GetSurface_SecondOverUniform (unsigned short val_marker) const |
| Get the relative secondary flow strength at the surface. More... | |
| su2double | GetSurface_MomentumDistortion (unsigned short val_marker) const |
| Get the momentum distortion at the surface. More... | |
| su2double | GetSurface_TotalTemperature (unsigned short val_marker) const |
| Get the total temperature at an outlet boundary. More... | |
| su2double | GetSurface_TotalPressure (unsigned short val_marker) const |
| Get the total pressure at an outlet boundary. More... | |
| su2double | GetSurface_PressureDrop (unsigned short val_marker) const |
| Get the pressure drop between two surfaces. More... | |
| su2double | GetSurface_Species_0 (unsigned short val_marker) const |
| Get avg species_0 at a boundary. More... | |
| su2double | GetSurface_Species_Variance (unsigned short val_marker) const |
| Get the species variance at a boundary. More... | |
| su2double | GetSurface_IDC (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetSurface_IDC_Mach (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetSurface_IDR (unsigned short val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_Pressure (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_TotalPressure (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_GrossThrust (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_Force (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_Power (const string &val_marker) const |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetActDiskOutlet_Thrust_BEM (string val_marker) const |
| Get the thrust at the actuator disk outlet boundary. More... | |
| su2double | GetActDiskOutlet_Torque_BEM (string val_marker) const |
| Get the torque at the actuator disk outlet boundary. More... | |
| void | SetActDiskOutlet_Pressure (unsigned short val_marker, su2double val_actdisk_press) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_TotalPressure (unsigned short val_marker, su2double val_actdisk_totalpress) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_GrossThrust (unsigned short val_marker, su2double val_actdisk_grossthrust) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_Force (unsigned short val_marker, su2double val_actdisk_force) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_Power (unsigned short val_marker, su2double val_actdisk_power) |
| Get the back pressure (static) at an outlet boundary. More... | |
| void | SetActDiskOutlet_Thrust_BEM (unsigned short val_marker, su2double val_actdisk_thrust_bem) |
| Set the thrust at the outlet (actuator disk) boundary. More... | |
| void | SetActDiskOutlet_Torque_BEM (unsigned short val_marker, su2double val_actdisk_torque_bem) |
| Get the back pressure (static) at an outlet boundary. More... | |
| su2double | GetDispl_Value (const string &val_index) const |
| Get the displacement value at an displacement boundary. More... | |
| su2double | GetLoad_Value (const string &val_index) const |
| Get the force value at an load boundary. More... | |
| su2double | GetDamper_Constant (const string &val_index) const |
| Get the constant value at a damper boundary. More... | |
| su2double | GetLoad_Dir_Value (const string &val_index) const |
| Get the force value at a load boundary defined in cartesian coordinates. More... | |
| su2double | GetLoad_Dir_Multiplier (const string &val_index) const |
| Get the force multiplier at a load boundary in cartesian coordinates. More... | |
| su2double | GetDisp_Dir_Value (const string &val_index) const |
| Get the force value at a load boundary defined in cartesian coordinates. More... | |
| su2double | GetDisp_Dir_Multiplier (const string &val_index) const |
| Get the force multiplier at a load boundary in cartesian coordinates. More... | |
| const su2double * | GetLoad_Dir (const string &val_index) const |
| Get the force direction at a loaded boundary in cartesian coordinates. More... | |
| const su2double * | GetDisp_Dir (const string &val_index) const |
| Get the force direction at a loaded boundary in cartesian coordinates. More... | |
| string | GetDV_Filename (void) const |
| Get name of the arbitrary mesh motion input file. More... | |
| string | GetDV_Unordered_Sens_Filename (void) const |
| Get name of the unordered ASCII volume sensitivity file. More... | |
| string | GetDV_Sens_Filename (void) const |
| Get name of the unordered ASCII surface sensitivity file. More... | |
| void | SetConfig_Options () |
| Set the config options. More... | |
| void | SetConfig_Parsing (char case_filename[MAX_STRING_SIZE]) |
| Set the config file parsing. More... | |
| void | SetConfig_Parsing (istream &config_buffer) |
| Set the config file parsing. More... | |
| bool | SetRunTime_Parsing (char case_filename[MAX_STRING_SIZE]) |
| Set the config file parsing. More... | |
| void | SetPostprocessing (SU2_COMPONENT val_software, unsigned short val_izone, unsigned short val_nDim) |
| Config file postprocessing. More... | |
| void | SetMarkers (SU2_COMPONENT val_software) |
| Config file markers processing. More... | |
| void | SetOutput (SU2_COMPONENT val_software, unsigned short val_izone) |
| Config file output. More... | |
| vector< vector< su2double > > | GetAeroelastic_np1 (unsigned short iMarker) const |
| Value of Aeroelastic solution coordinate at time n+1. More... | |
| vector< vector< su2double > > | GetAeroelastic_n (unsigned short iMarker) const |
| Value of Aeroelastic solution coordinate at time n. More... | |
| vector< vector< su2double > > | GetAeroelastic_n1 (unsigned short iMarker) const |
| Value of Aeroelastic solution coordinate at time n-1. More... | |
| void | SetAeroelastic_np1 (unsigned short iMarker, vector< vector< su2double > > solution) |
| Value of Aeroelastic solution coordinate at time n+1. More... | |
| void | SetAeroelastic_n (void) |
| Value of Aeroelastic solution coordinate at time n from time n+1. More... | |
| void | SetAeroelastic_n1 (void) |
| Value of Aeroelastic solution coordinate at time n-1 from time n. More... | |
| su2double | GetAeroelastic_Flutter_Speed_Index (void) const |
| Aeroelastic Flutter Speed Index. More... | |
| su2double | GetAeroelastic_Frequency_Plunge (void) const |
| Uncoupled Aeroelastic Frequency Plunge. More... | |
| su2double | GetAeroelastic_Frequency_Pitch (void) const |
| Uncoupled Aeroelastic Frequency Pitch. More... | |
| su2double | GetAeroelastic_Airfoil_Mass_Ratio (void) const |
| Aeroelastic Airfoil Mass Ratio. More... | |
| su2double | GetAeroelastic_CG_Location (void) const |
| Aeroelastic center of gravity location. More... | |
| su2double | GetAeroelastic_Radius_Gyration_Squared (void) const |
| Aeroelastic radius of gyration squared. More... | |
| unsigned short | GetAeroelasticIter (void) const |
| Aeroelastic solve every x inner iteration. More... | |
| su2double | GetAeroelastic_plunge (unsigned short val_marker) const |
| Value of plunging coordinate. More... | |
| su2double | GetAeroelastic_pitch (unsigned short val_marker) const |
| Value of pitching coordinate. More... | |
| void | SetAeroelastic_plunge (unsigned short val_marker, su2double val) |
| Value of plunging coordinate. More... | |
| void | SetAeroelastic_pitch (unsigned short val_marker, su2double val) |
| Value of pitching coordinate. More... | |
| bool | GetAeroelastic_Simulation (void) const |
| Get information about the aeroelastic simulation. More... | |
| bool | GetWind_Gust (void) const |
| Get information about the wind gust. More... | |
| unsigned short | GetGust_Type (void) const |
| Get the type of gust to simulate. More... | |
| unsigned short | GetGust_Dir (void) const |
| Get the gust direction. More... | |
| su2double | GetGust_WaveLength (void) const |
| Value of the gust wavelength. More... | |
| su2double | GetGust_Periods (void) const |
| Value of the number of gust periods. More... | |
| su2double | GetGust_Ampl (void) const |
| Value of the gust amplitude. More... | |
| su2double | GetGust_Begin_Time (void) const |
| Value of the time at which to begin the gust. More... | |
| su2double | GetGust_Begin_Loc (void) const |
| Value of the location ath which the gust begins. More... | |
| bool | GetTurb_Fixed_Values (void) const |
| Get whether fixed values for turbulence quantities are applied. More... | |
| su2double | GetTurb_Fixed_Values_MaxScalarProd (void) const |
| Get shift of the upstream half-plane where fixed values for turbulence quantities are applied. More... | |
| unsigned short | GetnFFD_Iter (void) const |
| Get the number of iterations to evaluate the parametric coordinates. More... | |
| su2double | GetFFD_Tol (void) const |
| Get the tolerance of the point inversion algorithm. More... | |
| tuple< bool, unsigned short, unsigned short > | GetFFD_IntPrev (void) const |
| Get information about whether to do a check on self-intersections within the FFD box based on value on the Jacobian determinant. More... | |
| tuple< bool, unsigned short, unsigned short > | GetConvexityCheck (void) const |
| Get information about whether to do a check on convexity of the mesh elements. More... | |
| su2double | GetOpt_RelaxFactor (void) const |
| Get the scale factor for the line search. More... | |
| su2double | GetOpt_LineSearch_Bound (void) const |
| Get the bound for the line search. More... | |
| void | SetOpt_RelaxFactor (su2double val_scale) |
| Set the scale factor for the line search. More... | |
| long | GetVisualize_CV (void) const |
| Get the node number of the CV to visualize. More... | |
| bool | GetFixed_CL_Mode (void) const |
| Get information about whether to use fixed CL mode. More... | |
| bool | GetEval_dOF_dCX (void) const |
| Get information about whether to use fixed CL mode. More... | |
| bool | GetDiscard_InFiles (void) const |
| Get information about whether to use fixed CL mode. More... | |
| su2double | GetTarget_CL (void) const |
| Get the value specified for the target CL. More... | |
| su2double | GetdCL_dAlpha (void) const |
| Get the value for the lift curve slope for fixed CL mode. More... | |
| unsigned long | GetIter_dCL_dAlpha (void) const |
| Number of iterations to evaluate dCL_dAlpha. More... | |
| unsigned long | GetIter_Fixed_NetThrust (void) const |
| Get the value of iterations to re-evaluate the angle of attack. More... | |
| su2double | GetdNetThrust_dBCThrust (void) const |
| Get the value of NetThrust_dBCThrust. More... | |
| unsigned long | GetUpdate_BCThrust (void) const |
| Get the value of iterations to re-evaluate the angle of attack. More... | |
| void | SetUpdate_BCThrust_Bool (bool val_update) |
| Set the value of the boolean for updating AoA in fixed lift mode. More... | |
| void | SetUpdate_AoA (bool val_update) |
| Set the value of the boolean for updating AoA in fixed lift mode. More... | |
| bool | GetUpdate_BCThrust_Bool (void) const |
| Get information about whether to update the AoA for fixed lift mode. More... | |
| bool | GetUpdate_AoA (void) const |
| Get information about whether to update the AoA for fixed lift mode. More... | |
| unsigned long | GetUpdate_AoA_Iter_Limit (void) const |
| Get the maximum number of iterations between AoA updates for fixed C_L mode. More... | |
| bool | GetFinite_Difference_Mode (void) const |
| Get whether at the end of finite differencing (Fixed CL mode) More... | |
| void | SetFinite_Difference_Mode (bool val_fd_mode) |
| Set whether at the end of finite differencing (Fixed CL mode) More... | |
| void | SetNonphysical_Points (unsigned long val_nonphys_points) |
| Set the current number of non-physical nodes in the solution. More... | |
| unsigned long | GetNonphysical_Points (void) const |
| Get the current number of non-physical nodes in the solution. More... | |
| void | SetNonphysical_Reconstr (unsigned long val_nonphys_reconstr) |
| Set the current number of non-physical reconstructions for 2nd-order upwinding. More... | |
| unsigned long | GetNonphysical_Reconstr (void) const |
| Get the current number of non-physical reconstructions for 2nd-order upwinding. More... | |
| void | Tick (double *val_start_time) |
| Start the timer for profiling subroutines. More... | |
| void | Tock (double val_start_time, const string &val_function_name, int val_group_id) |
| Stop the timer for profiling subroutines and store results. More... | |
| void | SetProfilingCSV (void) |
| Write a CSV file containing the results of the profiling. More... | |
| void | GEMM_Tick (double *val_start_time) const |
| Start the timer for profiling subroutines. More... | |
| void | GEMM_Tock (double val_start_time, int M, int N, int K) const |
| Stop the timer for the GEMM profiling and store results. More... | |
| void | GEMMProfilingCSV (void) |
| Write a CSV file containing the results of the profiling. More... | |
| void | SetFreeStreamTurboNormal (const su2double *turboNormal) |
| Set freestream turbonormal for initializing solution. More... | |
| const su2double * | GetFreeStreamTurboNormal (void) const |
| Set freestream turbonormal for initializing solution. More... | |
| void | SetMultizone (const CConfig *driver_config, const CConfig *const *config_container) |
| Set multizone properties. More... | |
| unsigned short | GetConsole_Output_Verb (void) const |
| Get the verbosity level of the console output. More... | |
| unsigned short | GetKind_Average (void) const |
| Get the kind of marker analyze marker (area-averaged, mass flux averaged, etc). More... | |
| unsigned short | GetDirectDiff () const |
| Get the direct differentation method. More... | |
| bool | GetDiscrete_Adjoint (void) const |
| Get the indicator whether we are solving an discrete adjoint problem. More... | |
| unsigned short | GetnIterFSI_Ramp (void) const |
| Get the number of subiterations while a ramp is applied. More... | |
| su2double | GetAitkenStatRelax (void) const |
| Get Aitken's relaxation parameter for static relaxation cases. More... | |
| su2double | GetAitkenDynMaxInit (void) const |
| Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration. More... | |
| su2double | GetAitkenDynMinInit (void) const |
| Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration. More... | |
| bool | GetDeadLoad (void) const |
| Decide whether to apply dead loads to the model. More... | |
| bool | GetPseudoStatic (void) const |
| Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures). More... | |
| bool | GetSteadyRestart (void) const |
| Identifies if we want to restart from a steady or an unsteady solution. More... | |
| unsigned short | GetiInst (void) const |
| Get the current instance. More... | |
| void | SetiInst (unsigned short val_iInst) |
| Set the current instance. More... | |
| su2double | GetNewmark_beta (void) const |
| Get Newmark alpha parameter. More... | |
| su2double | GetNewmark_gamma (void) const |
| Get Newmark delta parameter. More... | |
| unsigned short | GetnIntCoeffs (void) const |
| Get the number of integration coefficients provided by the user. More... | |
| unsigned short | GetnElasticityMat (void) const |
| Get the number of different materials for the elasticity solver. More... | |
| su2double | Get_Int_Coeffs (unsigned short val_coeff) const |
| Get the integration coefficients for the Generalized Alpha - Newmark integration integration scheme. More... | |
| unsigned short | GetnElectric_Field (void) const |
| Get the number of different values for the modulus of the electric field. More... | |
| unsigned short | GetnDim_Electric_Field (void) const |
| Get the dimensionality of the electric field. More... | |
| su2double | Get_Electric_Field_Mod (unsigned short val_coeff) const |
| Get the values for the electric field modulus. More... | |
| void | Set_Electric_Field_Mod (unsigned short val_coeff, su2double val_el_field) |
| Set the values for the electric field modulus. More... | |
| const su2double * | Get_Electric_Field_Dir (void) const |
| Get the direction of the electric field in reference configuration. More... | |
| bool | GetRamp_Load (void) const |
| Check if the user wants to apply the load as a ramp. More... | |
| su2double | GetRamp_Time (void) const |
| Get the maximum time of the ramp. More... | |
| bool | GetRampAndRelease_Load (void) const |
| Check if the user wants to apply the load as a ramp. More... | |
| bool | GetSine_Load (void) const |
| Check if the user wants to apply the load as a ramp. More... | |
| const su2double * | GetLoad_Sine (void) const |
| Get the sine load properties. More... | |
| unsigned short | GetDynamic_LoadTransfer (void) const |
| Get the kind of load transfer method we want to use for dynamic problems. More... | |
| su2double | GetRefGeom_Penalty (void) const |
| Get the penalty weight value for the objective function. More... | |
| su2double | GetTotalDV_Penalty (void) const |
| Get the penalty weight value for the objective function. More... | |
| array< su2double, 2 > | GetStressPenaltyParam (void) const |
| Get the maximum allowed VM stress and KS exponent for the stress penalty objective function. More... | |
| bool | GetPredictor (void) const |
| Get whether a predictor is used for FSI applications. More... | |
| unsigned short | GetPredictorOrder (void) const |
| Get the order of the predictor for FSI applications. More... | |
| bool | GetEulerPersson (void) const |
| Get boolean for using Persson's shock capturing method in Euler flow DG-FEM. More... | |
| void | SetEulerPersson (bool val_EulerPersson) |
| Set boolean for using Persson's shock capturing method in Euler flow DG-FEM. More... | |
| bool | GetRelaxation (void) const |
| Get whether a relaxation parameter is used for FSI applications. More... | |
| bool | GetFSI_Simulation (void) const |
| Check if the simulation we are running is a FSI simulation. More... | |
| void | SetMultizone_Problem (bool MZ_problem) |
| Set that the simulation we are running is a multizone simulation. More... | |
| bool | GetMultizone_Problem (void) const |
| Get whether the simulation we are running is a multizone simulation. More... | |
| unsigned short | GetnID_DV (void) const |
| Get the ID for the FEA region that we want to compute the gradient for using direct differentiation. More... | |
| bool | GetIncrementalLoad (void) const |
| Check if we want to apply an incremental load to the nonlinear structural simulation. More... | |
| unsigned long | GetNumberIncrements (void) const |
| Get the number of increments for an incremental load. More... | |
| su2double | GetIncLoad_Criteria (unsigned short val_var) const |
| Get the value of the criteria for applying incremental loading. More... | |
| BGS_RELAXATION | GetRelaxation_Method_BGS (void) const |
| Get the relaxation method chosen for the simulation. More... | |
| UPWIND | GetRiemann_Solver_FEM (void) const |
| Get the kind of Riemann solver for the DG method (FEM flow solver). More... | |
| su2double | GetQuadrature_Factor_Straight (void) const |
| Get the factor applied during quadrature of straight elements. More... | |
| su2double | GetQuadrature_Factor_Curved (void) const |
| Get the factor applied during quadrature of curved elements. More... | |
| su2double | GetQuadrature_Factor_Time_ADER_DG (void) const |
| Get the factor applied during time quadrature for ADER-DG. More... | |
| su2double | GetTheta_Interior_Penalty_DGFEM (void) const |
| Function to make available the multiplication factor theta of the symmetrizing terms in the DG discretization of the viscous terms. More... | |
| unsigned short | GetSizeMatMulPadding (void) const |
| Function to make available the matrix size in vectorization in order to optimize the gemm performance. More... | |
| bool | GetCompute_Entropy (void) const |
| Function to make available whether or not the entropy must be computed. More... | |
| bool | GetUse_Lumped_MassMatrix_DGFEM (void) const |
| Function to make available whether or not the lumped mass matrix must be used for steady computations. More... | |
| bool | GetJacobian_Spatial_Discretization_Only (void) const |
| Function to make available whether or not only the exact Jacobian of the spatial discretization must be computed. More... | |
| INTERFACE_INTERPOLATOR | GetKindInterpolation (void) const |
| Get the interpolation method used for matching between zones. More... | |
| bool | GetConservativeInterpolation (void) const |
| Get option of whether to use conservative interpolation between zones. More... | |
| RADIAL_BASIS | GetKindRadialBasisFunction (void) const |
| Get the basis function to use for radial basis function interpolation for FSI. More... | |
| bool | GetRadialBasisFunctionPolynomialOption (void) const |
| Get option of whether to use polynomial terms in Radial Basis Function interpolation. More... | |
| su2double | GetRadialBasisFunctionParameter (void) const |
| Get the basis function radius to use for radial basis function interpolation for FSI. More... | |
| su2double | GetRadialBasisFunctionPruneTol (void) const |
| Get the tolerance used to prune the interpolation matrix (making it sparser). More... | |
| unsigned short | GetNumNearestNeighbors (void) const |
| Get the number of donor points to use in Nearest Neighbor interpolation. More... | |
| INLET_SPANWISE_INTERP | GetKindInletInterpolationFunction (void) const |
| Get the kind of inlet face interpolation function to use. More... | |
| INLET_INTERP_TYPE | GetKindInletInterpolationType (void) const |
| Get the kind of inlet face interpolation data type. More... | |
| bool | GetPrintInlet_InterpolatedData (void) const |
| Get whether to print inlet interpolated data or not. More... | |
| su2double | GetUQ_Delta_B (void) const |
| Get the amount of eigenvalue perturbation to be done. More... | |
| unsigned short | GetEig_Val_Comp (void) const |
| Get the kind of eigenspace perturbation to be done. More... | |
| su2double | GetUQ_URLX (void) const |
| Get the underelaxation factor. More... | |
| bool | GetUQ_Permute (void) const |
| Get information about eigenspace perturbation. More... | |
| bool | GetWall_Functions (void) const |
| Get information about whether to use wall functions. More... | |
| bool | GetAD_Mode (void) const |
| Get the AD support. More... | |
| void | SetMax_Vel2 (su2double val_max_vel2) |
| Set the maximum velocity^2 in the domain for the incompressible preconditioner. More... | |
| su2double | GetMax_Vel2 (void) const |
| Get the maximum velocity^2 in the domain for the incompressible preconditioner. More... | |
| void | SetRestart_Bandwidth_Agg (su2double val_restart_bandwidth_sum) |
| Set the sum of the bandwidth for writing binary restarts (to be averaged later). More... | |
| su2double | GetRestart_Bandwidth_Agg (void) const |
| Set the sum of the bandwidth for writing binary restarts (to be averaged later). More... | |
| unsigned short | GetKind_HybridRANSLES (void) const |
| Get the Kind of Hybrid RANS/LES. More... | |
| unsigned short | GetKind_RoeLowDiss (void) const |
| Get the Kind of Roe Low Dissipation Scheme for Unsteady flows. More... | |
| su2double | GetConst_DES (void) const |
| Get the DES Constant. More... | |
| bool | GetAD_Preaccumulation (void) const |
| Get if AD preaccumulation should be performed. More... | |
| bool | GetWeakly_Coupled_Heat (void) const |
| Get the heat equation. More... | |
| CHT_COUPLING | GetKind_CHT_Coupling () const |
| Get the CHT couling method. More... | |
| bool | GetIntegrated_HeatFlux () const |
| Check if values passed to the BC_HeatFlux-Routine are already integrated. More... | |
| bool | GetCompute_Average (void) const |
| Get Compute Average. More... | |
| VERIFICATION_SOLUTION | GetVerification_Solution (void) const |
| Get the verification solution. More... | |
| bool | GetTopology_Optimization (void) const |
| Get topology optimization. More... | |
| string | GetTopology_Optim_FileName (void) const |
| Get name of output file for topology optimization derivatives. More... | |
| su2double | GetSIMP_Exponent (void) const |
| Get exponent for density-based stiffness penalization. More... | |
| su2double | GetSIMP_MinStiffness (void) const |
| Get lower bound for density-based stiffness penalization. More... | |
| unsigned short | GetTopology_Optim_Num_Kernels (void) const |
| Number of kernels to use in filtering the design density field. More... | |
| void | GetTopology_Optim_Kernel (const unsigned short iKernel, ENUM_FILTER_KERNEL &type, su2double ¶m, su2double &radius) const |
| Get the i'th kernel to use, its parameter, and the radius. More... | |
| unsigned short | GetTopology_Search_Limit (void) const |
| Get the maximum "logical radius" (degree of neighborhood) to consider in the neighbor search. More... | |
| void | GetTopology_Optim_Projection (ENUM_PROJECTION_FUNCTION &type, su2double ¶m) const |
| Get the type and parameter for the projection function used in topology optimization. More... | |
| string | GetConfigFilename (unsigned short index) const |
| Get the filenames of the individual config files. More... | |
| unsigned short | GetnConfigFiles (void) const |
| Get the number of config files. More... | |
| bool | GetTime_Domain (void) const |
| Check if the multizone problem is solved for time domain. More... | |
| unsigned long | GetnInner_Iter (void) const |
| Get the number of inner iterations. More... | |
| unsigned long | GetnOuter_Iter (void) const |
| Get the number of outer iterations. More... | |
| unsigned long | GetnTime_Iter (void) const |
| Get the number of time iterations. More... | |
| void | SetnTime_Iter (unsigned long val_iter) |
| Set the number of time iterations. More... | |
| unsigned long | GetRestart_Iter (void) const |
| Get the restart iteration. More... | |
| su2double | GetTime_Step (void) const |
| Get the time step for multizone problems. More... | |
| su2double | GetMax_Time (void) const |
| Get the maximum simulation time for time-domain problems. More... | |
| unsigned short | GetComm_Level (void) const |
| Get the level of MPI communications to be performed. More... | |
| bool | GetMultizone_Mesh (void) const |
| Check if the mesh read supports multiple zones. More... | |
| bool | GetMultizone_Residual (void) const |
| Check if the mesh read supports multiple zones. More... | |
| RADIATION_MODEL | GetKind_RadiationModel (void) const |
| Get the Kind of Radiation model applied. More... | |
| P1_INIT | GetKind_P1_Init (void) const |
| Get the Kind of P1 initialization method applied. More... | |
| su2double | GetAbsorption_Coeff (void) const |
| Get the value of the absorption coefficient of the medium. More... | |
| su2double | GetScattering_Coeff (void) const |
| Get the value of the scattering coefficient of the medium. More... | |
| su2double | GetWall_Emissivity (const string &val_index) const |
| Get the wall emissivity at a boundary. More... | |
| bool | GetMarker_StrongBC (const string &val_index) const |
| Get if boundary is strong or weak. More... | |
| su2double | GetCFL_Rad (void) const |
| Get the value of the CFL condition for radiation solvers. More... | |
| bool | AddRadiation (void) const |
| Determines if radiation needs to be incorporated to the analysis. More... | |
| bool | GetWrt_ZoneConv (void) const |
| Check if the convergence history of each individual zone is written to screen. More... | |
| bool | GetWrt_ZoneHist (void) const |
| Check if the convergence history of each individual zone is written to file. More... | |
| bool | GetSpecial_Output (void) const |
| Check if the special output is written. More... | |
| bool | GetWrt_ForcesBreakdown (void) const |
| Check if the forces breakdown file is written. More... | |
| short | GetMeshBoxSize (unsigned short val_iDim) const |
| Get the number of grid points in the analytic RECTANGLE or BOX grid in the specified coordinate direction. More... | |
| su2double | GetMeshBoxLength (unsigned short val_iDim) const |
| Get the length of the analytic RECTANGLE or BOX grid in the specified coordinate direction. More... | |
| su2double | GetMeshBoxOffset (unsigned short val_iDim) const |
| Get the offset from 0.0 of the analytic RECTANGLE or BOX grid in the specified coordinate direction. More... | |
| unsigned short | GetnScreenOutput (void) const |
| Get the number of screen output variables requested (maximum 6) More... | |
| string | GetScreenOutput_Field (unsigned short iField) const |
| Get the screen output field iField. More... | |
| unsigned short | GetnHistoryOutput (void) const |
| Get the number of history output variables requested. More... | |
| string | GetHistoryOutput_Field (unsigned short iField) const |
| Get the history output field iField. More... | |
| unsigned short | GetnVolumeOutput (void) const |
| Get the number of history output variables requested. More... | |
| string | GetVolumeOutput_Field (unsigned short iField) const |
| Get the history output field iField. More... | |
| string | GetConv_Field (unsigned short iField) const |
| Get the convergence fields for monitoring. More... | |
| string | GetWndConv_Field (unsigned short iField) const |
| Get functional that is going to be used to evaluate the convergence of the windowed time average of the unsteady problem. More... | |
| unsigned short | GetWnd_Cauchy_Elems (void) const |
| Get the number of iterations that are considered in the Cauchy convergence criteria for the windowed time average of the unsteady problem. More... | |
| su2double | GetWnd_Cauchy_Eps (void) const |
| Get the value of convergence criteria for the Cauchy method for the time averaged windowed objective functions for unsteady flows. More... | |
| unsigned long | GetWnd_StartConv_Iter (void) const |
| Get the number of iterations that are not considered in the convergence criteria for the windowed average output function. More... | |
| bool | GetWnd_Cauchy_Crit (void) const |
| Get the boolean value, whether the the Cauchy method for the time averaged windowed objective functions for unsteady flows is used or not. More... | |
| unsigned short | GetnWndConv_Field () const |
| Get the number of convergence monitoring fields for time convergence monitoring. return Number of convergence monitoring fields. More... | |
| unsigned short | GetnConv_Field () const |
| Get the number of convergence monitoring fields for inner convergence monitoring. return Number of convergence monitoring fields. More... | |
| void | Set_StartTime (su2double starttime) |
| Set the start time to track a phase of the code (preprocessing, compute, output). More... | |
| su2double | Get_StartTime () const |
| Get the start time to track a phase of the code (preprocessing, compute, output). More... | |
| unsigned long | GetHistory_Wrt_Freq (unsigned short iter) const |
| GetHistory_Wrt_Freq_Inner. More... | |
| void | SetHistory_Wrt_Freq (unsigned short iter, unsigned long nIter) |
| SetHistory_Wrt_Freq_Inner. More... | |
| unsigned long | GetScreen_Wrt_Freq (unsigned short iter) const |
| GetScreen_Wrt_Freq_Inner. More... | |
| void | SetScreen_Wrt_Freq (unsigned short iter, unsigned long nIter) |
| SetScreen_Wrt_Freq_Inner. More... | |
| const OUTPUT_TYPE * | GetVolumeOutputFiles () const |
| GetVolumeOutputFiles. More... | |
| unsigned short | GetnVolumeOutputFiles () const |
| GetnVolumeOutputFiles. More... | |
| unsigned long | GetVolumeOutputFrequency (unsigned short iFile) const |
| GetVolumeOutputFrequency. More... | |
| unsigned long | GetPastixFactFreq (void) const |
| Get the desired factorization frequency for PaStiX. More... | |
| unsigned short | GetPastixVerbLvl (void) const |
| Get the desired level of verbosity for PaStiX. More... | |
| unsigned short | GetPastixFillLvl (void) const |
| Get the desired level of fill for the PaStiX ILU. More... | |
| bool | OptionIsSet (string option) const |
| Check if an option is present in the config file. More... | |
| const string & | GetCaseName () const |
| Get the name of the current case. More... | |
| unsigned long | GetLinear_Solver_Prec_Threads (void) const |
| Get the number of threads per rank to use for ILU and LU_SGS preconditioners. More... | |
| unsigned long | GetEdgeColoringGroupSize (void) const |
| Get the size of the edge groups colored for OpenMP parallelization of edge loops. More... | |
| bool | GetEdgeColoringRelaxDiscAdj () const |
| Check if the discrete adjoint is allowed to relax the coloring, that is, allow smaller edge color group sizes and allow more colors. More... | |
| passivedouble | GetParMETIS_Tolerance () const |
| Get the ParMETIS load balancing tolerance. More... | |
| long | GetParMETIS_PointWeight () const |
| Get the ParMETIS load balancing weight for points. More... | |
| long | GetParMETIS_EdgeWeight () const |
| Get the ParMETIS load balancing weight for edges. More... | |
| short | FindInterfaceMarker (unsigned short iInterface) const |
| Find the marker index (if any) that is part of a given interface pair. More... | |
| bool | GetSave_libROM (void) const |
| Get whether or not to save solution data to libROM. More... | |
| string | GetlibROMbase_FileName (void) const |
| Get the name of the file for libROM to save. More... | |
| POD_KIND | GetKind_PODBasis (void) const |
| Static or incremental toggle for POD basis generation type. More... | |
| unsigned short | GetMax_BasisDim (void) const |
| Get maximum number of POD basis dimensions (default: 100). More... | |
| unsigned short | GetRom_SaveFreq (void) const |
| Get frequency of unsteady time steps to save (default: 1). More... | |
| bool | GetSmoothGradient (void) const |
| Check if the gradient smoothing is active. More... | |
| su2double | GetSmoothingEps1 (void) const |
| Gets the factor epsilon in front of the Laplace term. More... | |
| su2double | GetSmoothingEps2 (void) const |
| Gets the factor zeta in front of the identity term. More... | |
| bool | GetSmoothSepDim (void) const |
| Check if we split in the dimensions. More... | |
| bool | GetSmoothOnSurface (void) const |
| Check if we assemble the operator on the surface. More... | |
| bool | GetDirichletSurfaceBound (void) const |
| Check if we use zero Dirichlet boundarys on the bound of the surface. More... | |
| ENUM_SOBOLEV_MODUS | GetSobMode (void) const |
| The modus of operation for the Sobolev solver. More... | |
| string | GetObjFunc_Hess_FileName (void) const |
| Get the name of the file with the hessian of the objective function. More... | |
| su2double | GetGrad_Linear_Solver_Error (void) const |
| Get min error of the linear solver for the gradient smoothing. More... | |
| unsigned short | GetKind_Grad_Linear_Solver (void) const |
| Get the kind of solver for the gradient smoothing. More... | |
| unsigned short | GetKind_Grad_Linear_Solver_Prec (void) const |
| Get the kind of preconditioner for the gradient smoothing. More... | |
| unsigned long | GetGrad_Linear_Solver_Iter (void) const |
| Get max number of iterations of the for the gradient smoothing. More... | |
| SST_ParsedOptions | GetSSTParsedOptions () const |
| Get parsed SST option data structure. More... | |
| SA_ParsedOptions | GetSAParsedOptions () const |
| Get parsed SA option data structure. More... | |
| LM_ParsedOptions | GetLMParsedOptions () const |
| Get parsed LM option data structure. More... | |
| template<class Tenum , class TField > | |
| void | addEnumOption (const string name, TField &option_field, const map< string, Tenum > &enum_map, Tenum default_value) |
| template<class Tenum , class TField > | |
| void | addEnumListOption (const string name, unsigned short &input_size, TField *&option_field, const map< string, Tenum > &enum_map) |
Static Public Member Functions | |
| static unsigned short | GetnZone (const string &val_mesh_filename, unsigned short val_format) |
| Gets the number of zones in the mesh file. More... | |
| static unsigned short | GetnDim (const string &val_mesh_filename, unsigned short val_format) |
| Gets the number of dimensions in the mesh file. More... | |
Public Attributes | |
| vector< string > | fields |
| Tags for the different fields in a restart file. More... | |
Main class for defining the problem; basically this class reads the configuration file, and stores all the information.
Definition at line 62 of file CConfig.hpp.
| CConfig::CConfig | ( | char | case_filename[MAX_STRING_SIZE], |
| SU2_COMPONENT | val_software, | ||
| bool | verb_high | ||
| ) |
Constructor of the class which reads the input file.
Definition at line 64 of file CConfig.cpp.
| CConfig::CConfig | ( | istream & | case_buffer, |
| SU2_COMPONENT | val_software, | ||
| bool | verb_high | ||
| ) |
Constructor of the class which takes an istream buffer containing the config options.
Definition at line 109 of file CConfig.cpp.
| CConfig::CConfig | ( | CConfig * | config, |
| char | case_filename[MAX_STRING_SIZE], | ||
| SU2_COMPONENT | val_software, | ||
| unsigned short | val_iZone, | ||
| unsigned short | val_nZone, | ||
| bool | verb_high | ||
| ) |
Constructor of the class which reads the input file and uses default options from another config.
Definition at line 145 of file CConfig.cpp.
| CConfig::CConfig | ( | char | case_filename[MAX_STRING_SIZE], |
| SU2_COMPONENT | val_software | ||
| ) |
Constructor of the class which reads the input file.
Definition at line 191 of file CConfig.cpp.
| CConfig::CConfig | ( | char | case_filename[MAX_STRING_SIZE], |
| CConfig * | config | ||
| ) |
Constructor of the class which reads the input file.
Definition at line 230 of file CConfig.cpp.
| CConfig::~CConfig | ( | void | ) |
Destructor of the class.
Definition at line 8108 of file CConfig.cpp.
| void CConfig::addEnumListOption | ( | const string | name, |
| unsigned short & | input_size, | ||
| TField *& | option_field, | ||
| const map< string, Tenum > & | enum_map | ||
| ) |
Definition at line 361 of file CConfig.cpp.
| void CConfig::addEnumOption | ( | const string | name, |
| TField & | option_field, | ||
| const map< string, Tenum > & | enum_map, | ||
| Tenum | default_value | ||
| ) |
Definition at line 352 of file CConfig.cpp.
|
inline |
Determines if radiation needs to be incorporated to the analysis.
Definition at line 9553 of file CConfig.hpp.
| short CConfig::FindInterfaceMarker | ( | unsigned short | iInterface | ) | const |
Find the marker index (if any) that is part of a given interface pair.
| [in] | iInterface | - Number of the interface pair being tested, starting at 0. |
Definition at line 9763 of file CConfig.cpp.
| void CConfig::GEMM_Tick | ( | double * | val_start_time | ) | const |
Start the timer for profiling subroutines.
| [in] | val_start_time | - the value of the start time. |
Definition at line 9961 of file CConfig.cpp.
| void CConfig::GEMM_Tock | ( | double | val_start_time, |
| int | M, | ||
| int | N, | ||
| int | K | ||
| ) | const |
Stop the timer for the GEMM profiling and store results.
| [in] | val_start_time | - The value of the start time. |
| [in] | M,N,K | - Matrix size of the GEMM call. |
Definition at line 9975 of file CConfig.cpp.
| void CConfig::GEMMProfilingCSV | ( | void | ) |
Write a CSV file containing the results of the profiling.
Definition at line 10023 of file CConfig.cpp.
|
inline |
Get the alpha (convective) coefficients for the Runge-Kutta integration scheme.
| [in] | val_step | - Index of the step. |
Definition at line 3347 of file CConfig.hpp.
|
inline |
Get the direction of the electric field in reference configuration.
| [in] | val_coeff | - Index of the coefficient. |
Definition at line 9023 of file CConfig.hpp.
|
inline |
Get the values for the electric field modulus.
| [in] | val_coeff | - Index of the coefficient. |
Definition at line 9009 of file CConfig.hpp.
|
inline |
Get the integration coefficients for the Generalized Alpha - Newmark integration integration scheme.
| [in] | val_coeff | - Index of the coefficient. |
Definition at line 8990 of file CConfig.hpp.
|
inline |
number span-wise sections to compute 3D BC and performance for turbomachinery specified by the user.
Definition at line 5305 of file CConfig.hpp.
|
inline |
Get the start time to track a phase of the code (preprocessing, compute, output).
Definition at line 9689 of file CConfig.hpp.
|
inline |
Get the value of the absorption coefficient of the medium.
Definition at line 9521 of file CConfig.hpp.
|
inline |
Get the value of the critical pressure.
Definition at line 4032 of file CConfig.hpp.
| su2double CConfig::GetActDisk_Area | ( | const string & | val_marker | ) | const |
Get the tip radius of th actuator disk.
Definition at line 8795 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7740 of file CConfig.hpp.
| su2double CConfig::GetActDisk_BCThrust | ( | const string & | val_marker | ) | const |
Get the origin of the actuator disk.
Definition at line 8763 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7719 of file CConfig.hpp.
| su2double CConfig::GetActDisk_BCThrust_Old | ( | const string & | val_marker | ) | const |
Get the origin of the actuator disk.
Definition at line 8771 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7726 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7670 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7677 of file CConfig.hpp.
|
inline |
Actuator disk defined with a double surface.
TRUE if the elements must be divided; otherwise FALSE. Definition at line 5870 of file CConfig.hpp.
|
inline |
Get name of the input file for the specified actuator disk.
Definition at line 5078 of file CConfig.hpp.
| su2double CConfig::GetActDisk_Force | ( | const string & | val_marker | ) | const |
Get the origin of the actuator disk.
Definition at line 8755 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8139 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7733 of file CConfig.hpp.
|
inline |
Get the format of the output solution.
Definition at line 5629 of file CConfig.hpp.
| su2double CConfig::GetActDisk_Mach | ( | const string & | val_marker | ) | const |
Get the origin of the actuator disk.
Definition at line 8747 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8132 of file CConfig.hpp.
| su2double CConfig::GetActDisk_MassFlow | ( | const string & | val_marker | ) | const |
Get the origin of the actuator disk.
Definition at line 8739 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8125 of file CConfig.hpp.
| su2double CConfig::GetActDisk_NetThrust | ( | const string & | val_marker | ) | const |
Get the origin of the actuator disk.
Definition at line 8723 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7712 of file CConfig.hpp.
| su2double CConfig::GetActDisk_Omega | ( | const string & | val_marker, |
| unsigned short | val_index | ||
| ) | const |
Get the rev / min of the actuator disk.
Definition at line 8827 of file CConfig.cpp.
| su2double CConfig::GetActDisk_Power | ( | const string & | val_marker | ) | const |
Get the origin of the actuator disk.
Definition at line 8731 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8118 of file CConfig.hpp.
| su2double CConfig::GetActDisk_PressJump | ( | const string & | val_marker, |
| unsigned short | val_index | ||
| ) | const |
Get the thrust corffient of the actuator disk.
Definition at line 8811 of file CConfig.cpp.
| su2double CConfig::GetActDisk_ReverseMassFlow | ( | const string & | val_marker | ) | const |
Get the tip radius of th actuator disk.
Definition at line 8803 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7747 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7698 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7705 of file CConfig.hpp.
|
inline |
Actuator disk defined with a double surface.
TRUE if the elements must be divided; otherwise FALSE. Definition at line 5882 of file CConfig.hpp.
| su2double CConfig::GetActDisk_TempJump | ( | const string & | val_marker, |
| unsigned short | val_index | ||
| ) | const |
Get the thrust corffient of the actuator disk.
Definition at line 8819 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7684 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7691 of file CConfig.hpp.
| su2double CConfig::GetActDiskBem_Axis | ( | unsigned short | iDim, |
| string | val_marker, | ||
| unsigned short | val_index | ||
| ) | const |
Get the axis of the actuator disk with BEM.
Definition at line 8843 of file CConfig.cpp.
| su2double CConfig::GetActDiskBem_CG | ( | unsigned short | iDim, |
| string | val_marker, | ||
| unsigned short | val_index | ||
| ) | const |
Get the Center of the actuator disk with BEM.
Definition at line 8835 of file CConfig.cpp.
|
inline |
Get the frequency of updating the actuator disk with BEM.
Definition at line 6772 of file CConfig.hpp.
| su2double CConfig::GetActDiskInlet_Force | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9578 of file CConfig.cpp.
| su2double CConfig::GetActDiskInlet_MassFlow | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9669 of file CConfig.cpp.
| su2double CConfig::GetActDiskInlet_Power | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9585 of file CConfig.cpp.
| su2double CConfig::GetActDiskInlet_Pressure | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9557 of file CConfig.cpp.
| su2double CConfig::GetActDiskInlet_RamDrag | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9571 of file CConfig.cpp.
| su2double CConfig::GetActDiskInlet_Temperature | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9641 of file CConfig.cpp.
| su2double CConfig::GetActDiskInlet_TotalPressure | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9564 of file CConfig.cpp.
| su2double CConfig::GetActDiskInlet_TotalTemperature | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9648 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_Force | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9613 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_GrossThrust | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9606 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_MassFlow | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9676 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_Power | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9620 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_Pressure | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9592 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_Temperature | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9655 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_Thrust_BEM | ( | string | val_marker | ) | const |
Get the thrust at the actuator disk outlet boundary.
| [in] | val_marker | - Marker corresponding to the outlet (actuator disk) boundary. |
Definition at line 9627 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_Torque_BEM | ( | string | val_marker | ) | const |
Get the torque at the actuator disk outlet boundary.
| [in] | val_marker | - Marker corresponding to the outlet boundary. |
Definition at line 9634 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_TotalPressure | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9599 of file CConfig.cpp.
| su2double CConfig::GetActDiskOutlet_TotalTemperature | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9662 of file CConfig.cpp.
|
inline |
Get the AD support.
Definition at line 9301 of file CConfig.hpp.
|
inline |
Get if AD preaccumulation should be performed.
Definition at line 9348 of file CConfig.hpp.
| bool CConfig::GetAdiabaticWall | ( | void | ) |
Get information about the adibatic wall condition.
TRUE if it is a adiabatic wall condition; otherwise FALSE.
|
inline |
Get the name of the file with the adjoint variables.
Definition at line 5728 of file CConfig.hpp.
|
inline |
Get the limit value for the adjoint variables.
Definition at line 1581 of file CConfig.hpp.
|
inline |
Get the value of sharp edge limiter.
Definition at line 2502 of file CConfig.hpp.
|
inline |
Determine if advanced features are used from the element-based FEA analysis (experimental feature).
TRUE is experimental, FALSE is the default behaviour. Definition at line 2372 of file CConfig.hpp.
|
inline |
Aeroelastic Airfoil Mass Ratio.
Definition at line 8547 of file CConfig.hpp.
|
inline |
Aeroelastic center of gravity location.
Definition at line 8552 of file CConfig.hpp.
|
inline |
Aeroelastic Flutter Speed Index.
Definition at line 8532 of file CConfig.hpp.
|
inline |
Uncoupled Aeroelastic Frequency Pitch.
Definition at line 8542 of file CConfig.hpp.
|
inline |
Uncoupled Aeroelastic Frequency Plunge.
Definition at line 8537 of file CConfig.hpp.
|
inline |
Value of Aeroelastic solution coordinate at time n.
Definition at line 8507 of file CConfig.hpp.
|
inline |
Value of Aeroelastic solution coordinate at time n-1.
Definition at line 8512 of file CConfig.hpp.
|
inline |
Value of Aeroelastic solution coordinate at time n+1.
Definition at line 8502 of file CConfig.hpp.
|
inline |
Value of pitching coordinate.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 8576 of file CConfig.hpp.
|
inline |
Value of plunging coordinate.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 8569 of file CConfig.hpp.
|
inline |
Aeroelastic radius of gyration squared.
Definition at line 8557 of file CConfig.hpp.
|
inline |
Get information about the aeroelastic simulation.
TRUE if it is an aeroelastic case; otherwise FALSE. Definition at line 8596 of file CConfig.hpp.
|
inline |
Aeroelastic solve every x inner iteration.
Definition at line 8562 of file CConfig.hpp.
|
inline |
Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration.
Definition at line 8923 of file CConfig.hpp.
|
inline |
Get Aitken's maximum relaxation parameter for dynamic relaxation cases and first iteration.
Definition at line 8929 of file CConfig.hpp.
|
inline |
Get Aitken's relaxation parameter for static relaxation cases.
Definition at line 8917 of file CConfig.hpp.
|
inline |
Get the angle of attack of the body. This is the angle between a reference line on a lifting body (often the chord line of an airfoil) and the vector representing the relative motion between the lifting body and the fluid through which it is moving.
Definition at line 2790 of file CConfig.hpp.
|
inline |
Get the off set angle of attack of the body. The solution and the geometry file are able to modifity the angle of attack in the config file.
Definition at line 2797 of file CConfig.hpp.
|
inline |
Get the functional sensitivity with respect to changes in the angle of attack.
Definition at line 2810 of file CConfig.hpp.
|
inline |
Get the angle of sideslip of the body. It relates to the rotation of the aircraft centerline from the relative wind.
Definition at line 2847 of file CConfig.hpp.
|
inline |
Get the off set sideslip angle of the body. The solution and the geometry file are able to modifity the angle of attack in the config file.
Definition at line 2804 of file CConfig.hpp.
|
inline |
Return true if an AUSM method is in use.
Definition at line 3892 of file CConfig.hpp.
|
inline |
Get mach limit for average massflow-based procedure .
Definition at line 5203 of file CConfig.hpp.
|
inline |
Get information about the axisymmetric frame.
TRUE if there is a rotational frame; otherwise FALSE. Definition at line 6319 of file CConfig.hpp.
|
inline |
Evaluation frequency for Engine and Actuator disk markers.
Definition at line 6554 of file CConfig.hpp.
|
inline |
Get the blade angle of the propeller.
Definition at line 6777 of file CConfig.hpp.
|
inline |
Get the filename of the propeller.
Definition at line 6782 of file CConfig.hpp.
|
inline |
Get the epsilon^2 multiplier for Beta in the incompressible preconditioner.
Definition at line 1676 of file CConfig.hpp.
|
inline |
Get information about the body force.
TRUE if it uses a body force; otherwise FALSE. Definition at line 6220 of file CConfig.hpp.
|
inline |
Get a pointer to the body force vector.
Definition at line 6226 of file CConfig.hpp.
|
inline |
Verify if there is any Giles Boundary Condition option specified from config file.
Definition at line 5269 of file CConfig.hpp.
|
inline |
Verify if there is mixing plane interface specified from config file.
Definition at line 5227 of file CConfig.hpp.
|
inline |
Verify if there is any Riemann Boundary Condition option specified from config file.
Definition at line 5275 of file CConfig.hpp.
|
inline |
Verify if there is mixing plane interface specified from config file.
Definition at line 5233 of file CConfig.hpp.
|
inline |
Verify if there is Turbomachinery performance option specified from config file.
Definition at line 5251 of file CConfig.hpp.
|
inline |
Returns true if bounded scalar mode is used for any equation.
Definition at line 4997 of file CConfig.hpp.
|
inline |
Returns true if bounded scalar mode is on for species transport.
Definition at line 4987 of file CConfig.hpp.
|
inline |
Returns true if bounded scalar mode is on for turbulence transport.
Definition at line 4992 of file CConfig.hpp.
|
inline |
Get the name of the file with the forces breakdown of the problem.
Definition at line 5654 of file CConfig.hpp.
|
inline |
Get the buffet sensor sharpness coefficient.
Definition at line 6344 of file CConfig.hpp.
|
inline |
Get the buffet sensor offset parameter.
Definition at line 6350 of file CConfig.hpp.
|
inline |
Get the value of the bulk modulus.
Definition at line 1670 of file CConfig.hpp.
|
inline |
Get the name of the current case.
Definition at line 9763 of file CConfig.hpp.
|
inline |
Determines if problem has catalytic walls.
Definition at line 6535 of file CConfig.hpp.
|
inline |
Get wall catalytic efficiency.
Definition at line 3951 of file CConfig.hpp.
| bool CConfig::GetCatalytic_Wall | ( | unsigned short | iMarker | ) | const |
Determines whether a marker with index iMarker is a catalytic boundary.
| iMarker |
Definition at line 8065 of file CConfig.cpp.
|
inline |
Get the number of iterations that are considered in the Cauchy convergence criteria.
Definition at line 5804 of file CConfig.hpp.
|
inline |
Get the value of convergence criteria for the Cauchy method in the direct, adjoint or linearized problem.
Definition at line 5817 of file CConfig.hpp.
|
inline |
Get functional that is going to be used to evaluate the adjoint flow convergence.
Definition at line 5798 of file CConfig.hpp.
|
inline |
Get functional that is going to be used to evaluate the flow convergence.
Definition at line 5792 of file CConfig.hpp.
|
inline |
Factor by which to multiply the dissipation contribution to Jacobians of incompressible central schemes.
Definition at line 4844 of file CConfig.hpp.
|
inline |
Factor by which to multiply the dissipation contribution to Jacobians of central schemes.
Definition at line 4838 of file CConfig.hpp.
|
inline |
Get the Courant Friedrich Levi number for each grid.
| [in] | val_mesh | - Index of the mesh were the CFL is applied. |
Definition at line 2897 of file CConfig.hpp.
|
inline |
Get the value of the CFL adaption flag.
TRUE if CFL adaption is active; otherwise FALSE. Definition at line 1652 of file CConfig.hpp.
|
inline |
Get the values of the CFL adaption parameters.
Definition at line 1646 of file CConfig.hpp.
|
inline |
Get the value of the CFL condition for radiation solvers.
Definition at line 9547 of file CConfig.hpp.
|
inline |
Get CFL reduction factor for adjoint turbulence model.
Definition at line 4406 of file CConfig.hpp.
|
inline |
Value of the CFL reduction in species problems.
Definition at line 6987 of file CConfig.hpp.
|
inline |
Value of the CFL reduction in turbulence problems.
Definition at line 6981 of file CConfig.hpp.
|
inline |
Get the charge coefficient that is used in the poissonal potential simulation.
Definition at line 2853 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6662 of file CConfig.hpp.
|
inline |
Get the level of MPI communications to be performed.
Definition at line 9491 of file CConfig.hpp.
|
inline |
Get Compute Average.
Definition at line 9372 of file CConfig.hpp.
|
inline |
Function to make available whether or not the entropy must be computed.
Definition at line 9202 of file CConfig.hpp.
|
inline |
Get the filenames of the individual config files.
Definition at line 9431 of file CConfig.hpp.
|
inline |
Get the value of the Confinement Parameter.
Definition at line 1640 of file CConfig.hpp.
|
inline |
Get option of whether to use conservative interpolation between zones.
Definition at line 9226 of file CConfig.hpp.
|
inline |
Get the verbosity level of the console output.
Definition at line 8887 of file CConfig.hpp.
|
inline |
|
inline |
Get the value of the Lewis number for each species.
Definition at line 4120 of file CConfig.hpp.
|
inline |
Get the contact resistance value of a specified interface.
| [in] | val_interface | interface index. |
Definition at line 3693 of file CConfig.hpp.
| unsigned short CConfig::GetContainerPosition | ( | unsigned short | val_eqsystem | ) |
Provides the index of the solution in the container.
| [in] | val_eqsystem | - Equation that is being solved. |
Definition at line 8521 of file CConfig.cpp.
|
inline |
Determines if problem is adjoint.
Definition at line 6523 of file CConfig.hpp.
|
inline |
Get the name of a specific controlling variable.
Definition at line 2227 of file CConfig.hpp.
|
inline |
Get the name of the source term variable for a specific controlling variable.
Definition at line 2234 of file CConfig.hpp.
|
inline |
Get the convergence fields for monitoring.
| [in] | iField | - Index of the field return Field name for monitoring convergence |
Definition at line 9632 of file CConfig.hpp.
|
inline |
Get the name of the file with the convergence history of the problem.
Definition at line 5635 of file CConfig.hpp.
|
inline |
Get information about whether to do a check on convexity of the mesh elements.
| [out] | ConvexityCheck | TRUE if convexity check is active; otherwise FALSE. |
| [out] | ConvexityCheck_MaxIter | Maximum number of iterations in the convexity check. |
| [out] | ConvexityCheck_MaxDepth | Maximum recursion depth in the convexity check. |
Definition at line 8684 of file CConfig.hpp.
|
inline |
Get the coordinates of the FFD corner points.
| [in] | val_ffd | - Index of the FFD box. |
| [in] | val_coord | - Index of the coordinate that we want to read. |
Definition at line 2938 of file CConfig.hpp.
|
inline |
Get the temperature polynomial coefficient for specific heat Cp.
| [in] | val_index | - Index of the array with all polynomial coefficients. |
Definition at line 4171 of file CConfig.hpp.
|
inline |
Get the temperature polynomial coefficient for specific heat Cp.
| [in] | val_index | - Index of the array with all polynomial coefficients. |
Definition at line 4178 of file CConfig.hpp.
|
inline |
If we are performing an unsteady simulation, this is the value of current time.
Definition at line 5858 of file CConfig.hpp.
|
inline |
Get the user expression for the custom objective function.
Definition at line 5442 of file CConfig.hpp.
|
inline |
Get the user expressions for custom outputs.
Definition at line 5447 of file CConfig.hpp.
|
inline |
Value of the damping factor for the correction prolongation.
Definition at line 6578 of file CConfig.hpp.
|
inline |
Value of the damping factor for the engine exhaust inlet bc.
Definition at line 6566 of file CConfig.hpp.
|
inline |
Value of the damping factor for the engine inlet bc.
Definition at line 6560 of file CConfig.hpp.
|
inline |
Value of the damping factor for the residual restriction.
Definition at line 6572 of file CConfig.hpp.
| su2double CConfig::GetDamper_Constant | ( | const string & | val_index | ) | const |
Get the constant value at a damper boundary.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 9697 of file CConfig.cpp.
|
inline |
Get name of the input file for the data-driven fluid model interpolation method.
Definition at line 3968 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6608 of file CConfig.hpp.
|
inline |
Get the value for the lift curve slope for fixed CL mode.
Definition at line 8740 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6620 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6632 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6644 of file CConfig.hpp.
|
inline |
Decide whether to apply DE effects to the model.
TRUE if the DE effects are to be applied, FALSE otherwise. Definition at line 2278 of file CConfig.hpp.
|
inline |
Decide whether to apply dead loads to the model.
TRUE if the dead loads are to be applied, FALSE otherwise. Definition at line 8935 of file CConfig.hpp.
|
inline |
Get factor to multiply smallest volume for deform tolerance.
Definition at line 4430 of file CConfig.hpp.
|
inline |
Get Young's modulus for deformation (constant stiffness deformation)
Definition at line 4441 of file CConfig.hpp.
|
inline |
Get limit for the volumetric deformation.
Definition at line 4436 of file CConfig.hpp.
|
inline |
Get min error of the linear solver for the implicit formulation.
Definition at line 4299 of file CConfig.hpp.
|
inline |
Get max number of iterations of the linear solver for the implicit formulation.
Definition at line 4311 of file CConfig.hpp.
|
inline |
Get information about whether the mesh will be deformed using pseudo linear elasticity.
TRUE means that grid deformation is active. Definition at line 4418 of file CConfig.hpp.
|
inline |
Get information about writing grid deformation residuals to the console.
TRUE means that grid deformation residuals will be written to the console. Definition at line 4424 of file CConfig.hpp.
|
inline |
Get Poisson's ratio for deformation (constant stiffness deformation) .
Definition at line 4447 of file CConfig.hpp.
|
inline |
Get the size of the layer of highest stiffness for wall distance-based mesh stiffness.
Definition at line 4458 of file CConfig.hpp.
|
inline |
Get the type of stiffness to impose for FEA mesh deformation.
Definition at line 4453 of file CConfig.hpp.
|
inline |
Get the degree of the FFD corner points.
| [in] | val_ffd | - Index of the FFD box. |
| [in] | val_degree | - Index (I,J,K) to obtain the degree. |
Definition at line 2946 of file CConfig.hpp.
|
inline |
If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.
Definition at line 5838 of file CConfig.hpp.
|
inline |
If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.
Definition at line 5824 of file CConfig.hpp.
|
inline |
Get the value of the freestream density.
Definition at line 1759 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream density.
Definition at line 1953 of file CConfig.hpp.
|
inline |
Get the value of the reference density for non-dimensionalization.
Definition at line 1856 of file CConfig.hpp.
|
inline |
Obtain the kind of design variable.
| [in] | val_dv | - Number of the design variable that we want to read. |
Definition at line 6338 of file CConfig.hpp.
|
inline |
Get the value of the constant mass diffusivity for scalar transport.
Definition at line 4096 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensional constant mass diffusivity.
Definition at line 4102 of file CConfig.hpp.
|
inline |
Get the direct differentation method.
Definition at line 8899 of file CConfig.hpp.
|
inline |
Check if we use zero Dirichlet boundarys on the bound of the surface.
Definition at line 9867 of file CConfig.hpp.
|
inline |
Get information about whether to use fixed CL mode.
TRUE if fixed CL mode is active; otherwise FALSE. Definition at line 8728 of file CConfig.hpp.
|
inline |
Get the indicator whether we are solving an discrete adjoint problem.
Definition at line 8905 of file CConfig.hpp.
| const su2double * CConfig::GetDisp_Dir | ( | const string & | val_index | ) | const |
Get the force direction at a loaded boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 9739 of file CConfig.cpp.
| su2double CConfig::GetDisp_Dir_Multiplier | ( | const string & | val_index | ) | const |
Get the force multiplier at a load boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 9725 of file CConfig.cpp.
| su2double CConfig::GetDisp_Dir_Value | ( | const string & | val_index | ) | const |
Get the force value at a load boundary defined in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 9718 of file CConfig.cpp.
| su2double CConfig::GetDispl_Value | ( | const string & | val_index | ) | const |
Get the displacement value at an displacement boundary.
| [in] | val_index | - Index corresponding to the displacement boundary. |
Definition at line 9683 of file CConfig.cpp.
|
inline |
|
inline |
Get the value of NetThrust_dBCThrust.
Definition at line 8758 of file CConfig.hpp.
|
inline |
Get the volume of the whole domain using the fine grid, this value is common for all the grids in the multigrid method.
Definition at line 2433 of file CConfig.hpp.
|
inline |
Get the kind of design variable for FEA.
Definition at line 2308 of file CConfig.hpp.
|
inline |
Get name of the arbitrary mesh motion input file.
Definition at line 8450 of file CConfig.hpp.
|
inline |
Get name of the unordered ASCII surface sensitivity file.
Definition at line 8462 of file CConfig.hpp.
|
inline |
Get name of the unordered ASCII volume sensitivity file.
Definition at line 8456 of file CConfig.hpp.
|
inline |
Value of the design variable step, we use this value in design problems.
| [in] | val_dv | - Number of the design variable that we want to read. |
| [in] | val_val | - Value of the design variable that we want to read. |
Definition at line 5890 of file CConfig.hpp.
|
inline |
Definition at line 5891 of file CConfig.hpp.
|
inline |
Get information about dynamic grids.
TRUE if there is a grid movement; otherwise FALSE. Definition at line 5913 of file CConfig.hpp.
|
inline |
Get the kind of load transfer method we want to use for dynamic problems.
Definition at line 9062 of file CConfig.hpp.
|
inline |
Get the integration limits for the equivalent area computation.
| [in] | index | - 0 means x_min, and 1 means x_max. |
Definition at line 1568 of file CConfig.hpp.
|
inline |
Get the integration limits for the equivalent area computation.
| [in] | index | - 0 means x_min, and 1 means x_max. |
Definition at line 1575 of file CConfig.hpp.
|
inline |
Get the size of the edge groups colored for OpenMP parallelization of edge loops.
Definition at line 9774 of file CConfig.hpp.
|
inline |
Check if the discrete adjoint is allowed to relax the coloring, that is, allow smaller edge color group sizes and allow more colors.
Definition at line 9779 of file CConfig.hpp.
|
inline |
Get the kind of eigenspace perturbation to be done.
Definition at line 9278 of file CConfig.hpp.
|
inline |
Formulation for 2D elasticity (plane stress - strain)
Definition at line 2354 of file CConfig.hpp.
|
inline |
Get the Young's modulus of elasticity.
Definition at line 2272 of file CConfig.hpp.
|
inline |
Get the value of the DE modulus.
Definition at line 2290 of file CConfig.hpp.
|
inline |
Flag for whether to solve the energy equation for incompressible flows.
Definition at line 4003 of file CConfig.hpp.
|
inline |
Get the value of the freestream energy.
Definition at line 1747 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream energy.
Definition at line 1966 of file CConfig.hpp.
|
inline |
Get the value of the reference energy for non-dimensionalization.
Definition at line 1838 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
Definition at line 7565 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
Definition at line 7536 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
Definition at line 7558 of file CConfig.hpp.
|
inline |
Only halg of the engine is in the compputational grid.
TRUE if the engine is complete; otherwise FALSE. Definition at line 5876 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
Definition at line 7529 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
Definition at line 7551 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
Definition at line 7543 of file CConfig.hpp.
| su2double CConfig::GetEngineInflow_Target | ( | const string & | val_marker | ) | const |
Get the target (pressure, massflow, etc) at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
Definition at line 9424 of file CConfig.cpp.
|
inline |
Get the entropy fix.
Definition at line 4400 of file CConfig.hpp.
|
inline |
Information about computing and plotting the equivalent area distribution.
TRUE or FALSE depending if we are computing the equivalent area. Definition at line 5566 of file CConfig.hpp.
|
inline |
Get boolean for using Persson's shock capturing method in Euler flow DG-FEM.
Definition at line 9097 of file CConfig.hpp.
|
inline |
Get information about whether to use fixed CL mode.
TRUE if fixed CL mode is active; otherwise FALSE. Definition at line 8722 of file CConfig.hpp.
| su2double CConfig::GetExhaust_Force | ( | const string & | val_marker | ) | const |
Get the force balance at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9543 of file CConfig.cpp.
| su2double CConfig::GetExhaust_GrossThrust | ( | const string & | val_marker | ) | const |
Get the gross thrust at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9536 of file CConfig.cpp.
| su2double CConfig::GetExhaust_MassFlow | ( | const string & | val_marker | ) | const |
Get the massflow at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9515 of file CConfig.cpp.
| su2double CConfig::GetExhaust_Power | ( | const string & | val_marker | ) | const |
Get the power at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9550 of file CConfig.cpp.
| su2double CConfig::GetExhaust_Pressure | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9501 of file CConfig.cpp.
| su2double CConfig::GetExhaust_Pressure_Target | ( | const string & | val_index | ) | const |
Get the total pressure at an nacelle boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 8988 of file CConfig.cpp.
| su2double CConfig::GetExhaust_Temperature | ( | const string & | val_marker | ) | const |
Get the temperature (static) at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9508 of file CConfig.cpp.
| su2double CConfig::GetExhaust_Temperature_Target | ( | const string & | val_index | ) | const |
Get the total temperature at a nacelle boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 8981 of file CConfig.cpp.
| su2double CConfig::GetExhaust_TotalPressure | ( | const string & | val_marker | ) | const |
Get the total pressure at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9522 of file CConfig.cpp.
| su2double CConfig::GetExhaust_TotalTemperature | ( | const string & | val_marker | ) | const |
Get the total temperature at an engine exhaust boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9529 of file CConfig.cpp.
|
inline |
Get the current internal iteration number.
Definition at line 3275 of file CConfig.hpp.
|
inline |
Heat solver zone with extra screen output.
Definition at line 1622 of file CConfig.hpp.
|
inline |
Creates a tecplot file to visualize the partition made by the DDC software.
TRUE if the partition is going to be plotted; otherwise FALSE. Definition at line 1616 of file CConfig.hpp.
|
inline |
Get extra relaxation factor coefficients for the Giels BC.
Definition at line 5197 of file CConfig.hpp.
|
inline |
Get the value of the reference viscosity for non-dimensionalization.
Definition at line 1886 of file CConfig.hpp.
|
inline |
Get the name of the file with the element properties for structural problems.
Definition at line 2366 of file CConfig.hpp.
|
inline |
Return true if a high order FEM solver is in use.
Definition at line 3867 of file CConfig.hpp.
|
inline |
Get the value of the vector that connects the cartesian axis with a sherical or cylindrical one.
Definition at line 1664 of file CConfig.hpp.
|
inline |
Get the kind of FFD Blending function.
Definition at line 3011 of file CConfig.hpp.
|
inline |
Get the kind BSpline Order in i,j,k direction.
Definition at line 3017 of file CConfig.hpp.
|
inline |
Get the required continuity level at the surface intersection with the FFD.
Definition at line 2999 of file CConfig.hpp.
|
inline |
Get the coordinate system that we are going to use to define the FFD.
Definition at line 3005 of file CConfig.hpp.
|
inline |
plane of the FFD (I axis) that should be fixed.
| [in] | val_index | - Index of the arrray with all the planes in the I direction that should be fixed. |
Definition at line 3793 of file CConfig.hpp.
|
inline |
plane of the FFD (J axis) that should be fixed.
| [in] | val_index | - Index of the arrray with all the planes in the J direction that should be fixed. |
Definition at line 3800 of file CConfig.hpp.
|
inline |
plane of the FFD (K axis) that should be fixed.
| [in] | val_index | - Index of the arrray with all the planes in the K direction that should be fixed. |
Definition at line 3807 of file CConfig.hpp.
|
inline |
Get information about whether to do a check on self-intersections within the FFD box based on value on the Jacobian determinant.
| [out] | FFD_IntPrev | TRUE if FFD intersection prevention is active; otherwise FALSE. |
| [out] | FFD_IntPrev_MaxIter | Maximum number of iterations in the intersection prevention procedure. |
| [out] | FFD_IntPrev_MaxDepth | Maximum recursion depth in the intersection prevention procedure. |
Definition at line 8674 of file CConfig.hpp.
|
inline |
Define the FFD box with a symetry plane.
TRUE if there is a symmetry plane in the FFD; otherwise FALSE. Definition at line 4464 of file CConfig.hpp.
|
inline |
Get the tolerance of the point inversion algorithm.
Definition at line 8665 of file CConfig.hpp.
|
inline |
Get the FFD Tag of a particular design variable.
| [in] | val_dv | - Number of the design variable that we want to read. |
Definition at line 2953 of file CConfig.hpp.
| string CConfig::GetFilename | ( | string | filename, |
| const string & | ext, | ||
| int | Iter | ||
| ) | const |
Add any numbers necessary to the filename (iteration number, zone ID ...)
| [in] | filename | - the base filename. |
| [in] | ext | - the extension to be added. |
| [in] | Iter | - the current iteration |
Definition at line 8331 of file CConfig.cpp.
| string CConfig::GetFilename_Iter | ( | const string & | filename_iter, |
| unsigned long | curInnerIter, | ||
| unsigned long | curOuterIter | ||
| ) | const |
Add steady iteration number to the filename (does not overwrite previous files)
| [in] | filename | - the base filename. |
| [in] | inner_iter | - the inner iterations |
| [in] | outer_iter | - the outer iterations |
Definition at line 8358 of file CConfig.cpp.
|
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Get final Outlet Pressure value for the ramp.
Definition at line 5168 of file CConfig.hpp.
|
inline |
Get the angular velocity of the mesh about the z-axis.
Definition at line 6135 of file CConfig.hpp.
|
inline |
Get the index of the finest grid.
Definition at line 2877 of file CConfig.hpp.
|
inline |
Get whether at the end of finite differencing (Fixed CL mode)
Definition at line 8800 of file CConfig.hpp.
|
inline |
Value of the azimuthal line to fix due to a misalignments of the nearfield.
Definition at line 6602 of file CConfig.hpp.
|
inline |
Get information about whether to use fixed CL mode.
TRUE if fixed CL mode is active; otherwise FALSE. Definition at line 8716 of file CConfig.hpp.
|
inline |
Get the flame initialization. (x1,x2,x3) = flame offset/spark center location. (x4,x5,x6) = flame normal, separating unburnt from burnt or spark radius, spark start iteration, spark duration. (x7) = flame thickness, the length from unburnt to burnt conditions. (x8) = flame burnt thickness, the length to stay at burnt conditions.
Definition at line 2177 of file CConfig.hpp.
|
inline |
Get the ignition method used for combustion problems.
Definition at line 2256 of file CConfig.hpp.
| su2double CConfig::GetFlowAngleIn_BC | ( | ) | const |
Get the inlet flow angle imposed as BC for internal flow.
Definition at line 9254 of file CConfig.cpp.
|
inline |
Returns the name of the fluid we are using in CoolProp.
Definition at line 3985 of file CConfig.hpp.
|
inline |
Return true if a fluid solver is in use.
Definition at line 3837 of file CConfig.hpp.
|
inline |
Get the value of the reference force for non-dimensionalization.
Definition at line 1904 of file CConfig.hpp.
|
inline |
Set freestream turbonormal for initializing solution.
Definition at line 8876 of file CConfig.hpp.
|
inline |
Get the Froude number for free surface problems.
Definition at line 2516 of file CConfig.hpp.
|
inline |
Indicates whether the flow is frozen (chemistry deactivated).
Definition at line 5540 of file CConfig.hpp.
|
inline |
Provides information about the way in which the limiter will be treated by the disc. adjoint method.
FALSE means that the limiter computation is included. Definition at line 5048 of file CConfig.hpp.
|
inline |
Provides information about the way in which the turbulence will be treated by the cont. adjoint method.
FALSE means that the adjoint turbulence equations will be used. Definition at line 5028 of file CConfig.hpp.
|
inline |
Provides information about the way in which the turbulence will be treated by the disc. adjoint method.
FALSE means that the adjoint turbulence equations will be used. Definition at line 5035 of file CConfig.hpp.
|
inline |
Check if the simulation we are running is a FSI simulation.
Definition at line 9115 of file CConfig.hpp.
|
inline |
Get the value of the Gamma of fluid (ratio of specific heats).
Definition at line 1634 of file CConfig.hpp.
|
inline |
Provides the gas mass fractions of the flow.
Definition at line 5473 of file CConfig.hpp.
|
inline |
Get the value of specific gas constant.
Definition at line 1682 of file CConfig.hpp.
|
inline |
Get the reference value for the specific gas constant.
Definition at line 1724 of file CConfig.hpp.
|
inline |
Get the value of specific gas constant.
Definition at line 1688 of file CConfig.hpp.
|
inline |
Gas model that we are using.
Definition at line 3925 of file CConfig.hpp.
|
inline |
Get Description of the geometry to be analyzed.
Definition at line 1610 of file CConfig.hpp.
|
inline |
Get the location of the waterline.
Definition at line 5402 of file CConfig.hpp.
|
inline |
Geometric conditions for the structural solver.
Definition at line 2408 of file CConfig.hpp.
|
inline |
Get the king of evaluation in the geometrical module.
Definition at line 2890 of file CConfig.hpp.
| const su2double * CConfig::GetGiles_FlowDir | ( | const string & | val_marker | ) | const |
Get the Flowdir for the Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 9153 of file CConfig.cpp.
| su2double CConfig::GetGiles_RelaxFactorAverage | ( | const string & | val_marker | ) | const |
Get the relax factor for the average component for the Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 9139 of file CConfig.cpp.
| su2double CConfig::GetGiles_RelaxFactorFourier | ( | const string & | val_marker | ) | const |
Get the relax factor for the fourier component for the Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 9146 of file CConfig.cpp.
| su2double CConfig::GetGiles_Var1 | ( | const string & | val_marker | ) | const |
Get the var 1 for the Giels BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 9118 of file CConfig.cpp.
| su2double CConfig::GetGiles_Var2 | ( | const string & | val_marker | ) | const |
Get the var 2 for the Giles boundary.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 9132 of file CConfig.cpp.
|
inline |
Get min error of the linear solver for the gradient smoothing.
Definition at line 9885 of file CConfig.hpp.
|
inline |
Get max number of iterations of the for the gradient smoothing.
Definition at line 9903 of file CConfig.hpp.
|
inline |
Get information about the gravity force.
TRUE if it uses the gravity force; otherwise FALSE. Definition at line 6208 of file CConfig.hpp.
|
inline |
Get information about the grid movement.
TRUE if there is a grid movement; otherwise FALSE. Definition at line 5905 of file CConfig.hpp.
|
inline |
Get the number of nonlinear increments for mesh deformation.
Definition at line 4412 of file CConfig.hpp.
|
inline |
Value of the gust amplitude.
Definition at line 8629 of file CConfig.hpp.
|
inline |
Value of the location ath which the gust begins.
Definition at line 8639 of file CConfig.hpp.
|
inline |
Value of the time at which to begin the gust.
Definition at line 8634 of file CConfig.hpp.
|
inline |
|
inline |
Value of the number of gust periods.
Definition at line 8624 of file CConfig.hpp.
|
inline |
Get the type of gust to simulate.
Definition at line 8608 of file CConfig.hpp.
|
inline |
Value of the gust wavelength.
Definition at line 8619 of file CConfig.hpp.
|
inline |
Retrieves the period of oscillations to be used with Harmonic Balance.
Definition at line 3239 of file CConfig.hpp.
|
inline |
Get if harmonic balance source term is to be preconditioned.
Definition at line 6153 of file CConfig.hpp.
|
inline |
Get the reference value for the heat flux.
Definition at line 1730 of file CConfig.hpp.
|
inline |
Return true if a heat solver is in use.
Definition at line 3860 of file CConfig.hpp.
|
inline |
Get information about the volumetric heat source.
TRUE if it uses a volumetric heat source; otherwise FALSE. Definition at line 6267 of file CConfig.hpp.
|
inline |
Get the radius of the ellipsoid that introduces a volumetric heat source.
Definition at line 6307 of file CConfig.hpp.
|
inline |
Get the position of the center of the volumetric heat source.
Definition at line 6291 of file CConfig.hpp.
|
inline |
Get the rotation angle of the volumetric heat source in axis Z.
Definition at line 6279 of file CConfig.hpp.
|
inline |
Get information about the volumetric heat source.
Definition at line 6273 of file CConfig.hpp.
|
inline |
Get the value of the reference viscosity for non-dimensionalization.
Definition at line 1880 of file CConfig.hpp.
|
inline |
GetHistory_Wrt_Freq_Inner.
Definition at line 9695 of file CConfig.hpp.
|
inline |
Get the history output field iField.
Definition at line 9615 of file CConfig.hpp.
|
inline |
Provides information about the the nodes that are going to be moved on a deformation volumetric grid deformation.
TRUE means that only the points on the FFD box will be moved. Definition at line 5409 of file CConfig.hpp.
|
inline |
Get the coordinates where of the box where the grid is going to be deformed.
Definition at line 1587 of file CConfig.hpp.
|
inline |
Get RMS roughness for Transtion model from config.
Definition at line 4518 of file CConfig.hpp.
|
inline |
Get the current instance.
Definition at line 8953 of file CConfig.hpp.
|
inline |
Get the value of the initial density for incompressible flows.
Definition at line 2124 of file CConfig.hpp.
|
inline |
Get the value of the reference density for custom incompressible non-dimensionalization.
Definition at line 2106 of file CConfig.hpp.
|
inline |
Get the damping factor applied to velocity updates at incompressible pressure inlets.
Definition at line 5114 of file CConfig.hpp.
|
inline |
Flag for whether the local boundary normal is used as the flow direction for an incompressible pressure inlet.
FALSE means the prescribed flow direction is used. Definition at line 5102 of file CConfig.hpp.
|
inline |
Get the damping factor applied to pressure updates at incompressible mass flow outlet.
Definition at line 5120 of file CConfig.hpp.
|
inline |
Get the value of the initial temperature for incompressible flows.
Definition at line 2136 of file CConfig.hpp.
|
inline |
Get the value of the reference temperature for custom incompressible non-dimensionalization.
Definition at line 2118 of file CConfig.hpp.
|
inline |
Get the value of the initial velocity for incompressible flows.
Definition at line 2130 of file CConfig.hpp.
|
inline |
Get the value of the reference velocity for custom incompressible non-dimensionalization.
Definition at line 2112 of file CConfig.hpp.
| su2double CConfig::GetIncInlet_BC | ( | ) | const |
Get the inlet velocity or pressure imposed for incompressible flow.
Definition at line 9275 of file CConfig.cpp.
|
inline |
Get the value of the criteria for applying incremental loading.
Definition at line 9151 of file CConfig.hpp.
|
inline |
Provides information about using an inconsistent (primal/dual) discrete adjoint formulation.
FALSE means that the adjoint use the same numerical methods than the primal problem. Definition at line 5041 of file CConfig.hpp.
| su2double CConfig::GetIncPressureOut_BC | ( | ) | const |
Get the outlet pressure imposed as BC for incompressible flow.
Definition at line 9314 of file CConfig.cpp.
|
inline |
Check if we want to apply an incremental load to the nonlinear structural simulation.
TRUE means that the load is to be applied in increments. Definition at line 9139 of file CConfig.hpp.
| su2double CConfig::GetIncTemperature_BC | ( | ) | const |
Get the inlet temperature imposed as BC for incompressible flow.
Definition at line 9299 of file CConfig.cpp.
| su2double CConfig::GetInflow_Force | ( | const string & | val_marker | ) | const |
Get the force balance at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9480 of file CConfig.cpp.
| su2double CConfig::GetInflow_Mach | ( | const string & | val_marker | ) | const |
Get the fan face Mach number at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9494 of file CConfig.cpp.
| su2double CConfig::GetInflow_MassFlow | ( | const string & | val_marker | ) | const |
Get the mass flow rate at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9438 of file CConfig.cpp.
| su2double CConfig::GetInflow_Power | ( | const string & | val_marker | ) | const |
Get the power at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9487 of file CConfig.cpp.
| su2double CConfig::GetInflow_Pressure | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9431 of file CConfig.cpp.
| su2double CConfig::GetInflow_RamDrag | ( | const string & | val_marker | ) | const |
Get the ram drag at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9473 of file CConfig.cpp.
| su2double CConfig::GetInflow_ReverseMassFlow | ( | const string & | val_marker | ) | const |
Get the percentage of reverse flow at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9445 of file CConfig.cpp.
|
inline |
Get the percentage of reverse flow at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
Definition at line 7256 of file CConfig.hpp.
| su2double CConfig::GetInflow_Temperature | ( | const string & | val_marker | ) | const |
Get the temperature (static) at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9459 of file CConfig.cpp.
| su2double CConfig::GetInflow_TotalPressure | ( | const string & | val_marker | ) | const |
Get the total pressure at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9452 of file CConfig.cpp.
| su2double CConfig::GetInflow_TotalTemperature | ( | const string & | val_marker | ) | const |
Get the total temperature at an engine inflow boundary.
| [in] | val_marker | - Name of the boundary. |
Definition at line 9466 of file CConfig.cpp.
|
inline |
Get the value of the non-dimensionalized actuator disk turbulence intensity.
Definition at line 2050 of file CConfig.hpp.
|
inline |
Get name of the input file for the specified inlet profile.
Definition at line 5072 of file CConfig.hpp.
|
inline |
Get the mass fraction vector for a NEMO inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 6933 of file CConfig.hpp.
| su2double CConfig::GetInlet_Pressure | ( | const string & | val_index | ) | const |
Get the pressure at a supersonic inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 9044 of file CConfig.cpp.
|
inline |
Check if the inlet profile(s) are specified in an input file.
Definition at line 5066 of file CConfig.hpp.
|
inline |
Get the tolerance used for matching two points on a specified inlet.
Definition at line 5084 of file CConfig.hpp.
| const su2double * CConfig::GetInlet_SpeciesVal | ( | const string & | val_index | ) | const |
Get the species values at an inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 9058 of file CConfig.cpp.
| su2double CConfig::GetInlet_Temperature | ( | const string & | val_index | ) | const |
Get the temperature at a supersonic inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 9037 of file CConfig.cpp.
|
inline |
Get the Tve value for a NEMO inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 6940 of file CConfig.hpp.
| const su2double * CConfig::GetInlet_TurbVal | ( | const string & | val_index | ) | const |
Get the turbulent properties values at an inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 9065 of file CConfig.cpp.
| const su2double * CConfig::GetInlet_Velocity | ( | const string & | val_index | ) | const |
Get the velocity vector at a supersonic inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 9051 of file CConfig.cpp.
| const su2double * CConfig::GetInletFlowDir | ( | const string & | val_index | ) | const |
Get the flow direction unit vector at an inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 9030 of file CConfig.cpp.
| su2double CConfig::GetInletPtotal | ( | const string & | val_index | ) | const |
Get the total pressure at an inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 9016 of file CConfig.cpp.
| su2double CConfig::GetInletTtotal | ( | const string & | val_index | ) | const |
Get the total temperature at an inlet boundary.
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 9009 of file CConfig.cpp.
|
inline |
Get the current FSI iteration number.
Definition at line 3287 of file CConfig.hpp.
|
inline |
Check if values passed to the BC_HeatFlux-Routine are already integrated.
Definition at line 9366 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream intermittency.
Definition at line 2002 of file CConfig.hpp.
|
inline |
Information about computing and plotting the equivalent area distribution.
TRUE or FALSE depending if we are computing the equivalent area. Definition at line 5572 of file CConfig.hpp.
|
inline |
Information about computing and plotting the equivalent area distribution.
TRUE or FALSE depending if we are computing the equivalent area. Definition at line 5578 of file CConfig.hpp.
|
inline |
Indicates whether electron gas is present in the gas mixture.
Definition at line 5545 of file CConfig.hpp.
| su2double CConfig::GetIsothermal_Temperature | ( | const string & | val_index | ) | const |
Get the wall temperature (static) at an isothermal boundary.
| [in] | val_index | - Index corresponding to the isothermal boundary. |
Definition at line 9337 of file CConfig.cpp.
| bool CConfig::GetIsothermalWall | ( | void | ) |
Get information about the isothermal wall condition.
TRUE if it is a isothermal wall condition; otherwise FALSE.
|
inline |
Number of iterations to average (reverse time integration).
Definition at line 3227 of file CConfig.hpp.
|
inline |
Number of iterations to evaluate dCL_dAlpha.
Definition at line 8746 of file CConfig.hpp.
|
inline |
Get the value of iterations to re-evaluate the angle of attack.
Definition at line 8752 of file CConfig.hpp.
|
inline |
Provides the number of varaibles.
Definition at line 5527 of file CConfig.hpp.
|
inline |
Function to make available whether or not only the exact Jacobian of the spatial discretization must be computed.
Definition at line 9216 of file CConfig.hpp.
|
inline |
Value of the calibrated constant for the low order method (center scheme).
Definition at line 4896 of file CConfig.hpp.
|
inline |
Value of the calibrated constant for the Lax method (center scheme).
Definition at line 4820 of file CConfig.hpp.
|
inline |
Value of the calibrated constant for the high order method (center scheme).
Definition at line 4884 of file CConfig.hpp.
|
inline |
Value of the calibrated constant for the JST method (center scheme).
Definition at line 4826 of file CConfig.hpp.
|
inline |
Value of the calibrated constant for the high order method (center scheme).
Definition at line 4890 of file CConfig.hpp.
|
inline |
Value of the calibrated constant for the JST method (center scheme).
Definition at line 4832 of file CConfig.hpp.
|
inline |
Get the k constant factor define a lower limit by multiplication with values in SST turbulence model.
Definition at line 2026 of file CConfig.hpp.
|
inline |
Get the kind of inlet boundary condition treatment (total conditions or mass flow).
Definition at line 5379 of file CConfig.hpp.
|
inline |
Get the kind of scheme (aliased or non-aliased) to be used in the predictor step of ADER-DG.
Definition at line 4648 of file CConfig.hpp.
|
inline |
Get the kind of marker analyze marker (area-averaged, mass flux averaged, etc).
Definition at line 8893 of file CConfig.hpp.
|
inline |
Get the kind of mixing process for averaging quantities at the boundaries.
Definition at line 5126 of file CConfig.hpp.
|
inline |
Get kind of center scheme for the convective terms.
Definition at line 4557 of file CConfig.hpp.
|
inline |
Get the kind of center convective numerical scheme for the adjoint flow equations.
Definition at line 4870 of file CConfig.hpp.
|
inline |
Get the kind of center convective numerical scheme for the adjoint turbulence equations.
Definition at line 5013 of file CConfig.hpp.
|
inline |
Get the kind of center convective numerical scheme for the flow equations.
Definition at line 4737 of file CConfig.hpp.
|
inline |
Get the kind of center convective numerical scheme for the Species equations.
Definition at line 4974 of file CConfig.hpp.
| unsigned short CConfig::GetKind_Centered_Template | ( | void | ) |
Get the kind of center convective numerical scheme for the plasma equations.
|
inline |
Get the kind of center convective numerical scheme for the turbulence equations.
Definition at line 4922 of file CConfig.hpp.
|
inline |
Get the CHT couling method.
Definition at line 9360 of file CConfig.hpp.
|
inline |
Get the value of the thermal conductivity model.
Definition at line 4050 of file CConfig.hpp.
|
inline |
Get the value of the turbulent thermal conductivity model.
Definition at line 4056 of file CConfig.hpp.
|
inline |
Get the kind of convective numerical scheme.
Definition at line 4548 of file CConfig.hpp.
|
inline |
Get the kind of convective numerical scheme for the adjoint flow equations (centered or upwind).
Definition at line 4862 of file CConfig.hpp.
|
inline |
Get the kind of convective numerical scheme for the adjoint turbulence equations (centered or upwind).
Definition at line 4948 of file CConfig.hpp.
|
inline |
Get the kind of convective numerical scheme for the flow equations (finite element).
Definition at line 4720 of file CConfig.hpp.
|
inline |
Get the kind of convective numerical scheme for the flow equations (centered or upwind).
Definition at line 4711 of file CConfig.hpp.
|
inline |
Get the kind of convective numerical scheme for the heat equation.
Definition at line 5005 of file CConfig.hpp.
|
inline |
Get the kind of convective numerical scheme for the Species equations (upwind).
Definition at line 4966 of file CConfig.hpp.
|
inline |
Get the kind of convective numerical scheme for the template equations (centered or upwind).
Definition at line 4729 of file CConfig.hpp.
|
inline |
Get the kind of convective numerical scheme for the turbulence equations (upwind).
Definition at line 4914 of file CConfig.hpp.
| unsigned short CConfig::GetKind_Data_Giles | ( | const string & | val_marker | ) | const |
Get Kind Data for the Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 9160 of file CConfig.cpp.
| unsigned short CConfig::GetKind_Data_Riemann | ( | const string & | val_marker | ) | const |
Get Kind Data of Riemann boundary.
| [in] | val_marker | - Index corresponding to the Riemann boundary. |
Definition at line 9111 of file CConfig.cpp.
|
inline |
Datadriven method for EoS evaluation.
Definition at line 3962 of file CConfig.hpp.
|
inline |
Get the kind of solver for the implicit solver.
Definition at line 4287 of file CConfig.hpp.
|
inline |
Get the kind of preconditioner for the implicit solver.
Definition at line 4394 of file CConfig.hpp.
|
inline |
Option to define the density model for incompressible flows.
Definition at line 3991 of file CConfig.hpp.
|
inline |
Get the value of the mass diffusivity model.
Definition at line 4062 of file CConfig.hpp.
|
inline |
Get the kind of preconditioner for the implicit solver.
Definition at line 4388 of file CConfig.hpp.
|
inline |
Get the kind of solver for the implicit solver.
Definition at line 4382 of file CConfig.hpp.
|
inline |
Get the kind of inlet boundary condition treatment (total conditions or mass flow).
Definition at line 5373 of file CConfig.hpp.
|
inline |
Get the kind of shock capturing method in FEM DG solver.
Definition at line 4769 of file CConfig.hpp.
|
inline |
Get the kind of finite element convective numerical scheme for the flow equations.
Definition at line 4761 of file CConfig.hpp.
|
inline |
Fluid model that we are using.
Definition at line 3957 of file CConfig.hpp.
|
inline |
free stream option to initialize the solution
Definition at line 4009 of file CConfig.hpp.
|
inline |
Get the kind of solver for the gradient smoothing.
Definition at line 9891 of file CConfig.hpp.
|
inline |
Get the kind of preconditioner for the gradient smoothing.
Definition at line 9897 of file CConfig.hpp.
|
inline |
Get the kind of method for computation of spatial gradients used for viscous and source terms.
Definition at line 4250 of file CConfig.hpp.
|
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Get the kind of method for computation of spatial gradients used for upwind reconstruction.
Definition at line 4256 of file CConfig.hpp.
|
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Get the type of dynamic mesh motion. Each zone gets a config file.
Definition at line 5940 of file CConfig.hpp.
|
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Get the Kind of Hybrid RANS/LES.
Definition at line 9331 of file CConfig.hpp.
| INLET_TYPE CConfig::GetKind_Inc_Inlet | ( | const string & | val_marker | ) | const |
Get the type of incompressible inlet from the list.
Definition at line 8995 of file CConfig.cpp.
| INC_OUTLET_TYPE CConfig::GetKind_Inc_Outlet | ( | const string & | val_marker | ) | const |
Get the type of incompressible outlet from the list.
Definition at line 9002 of file CConfig.cpp.
|
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free stream option to initialize the solution
Definition at line 4015 of file CConfig.hpp.
|
inline |
Get the kind of inlet boundary condition treatment (total conditions or mass flow).
Definition at line 5060 of file CConfig.hpp.
|
inline |
Get the kind of solver for the implicit solver.
Definition at line 4274 of file CConfig.hpp.
|
inline |
Get the kind of preconditioner for the implicit solver.
Definition at line 4281 of file CConfig.hpp.
|
inline |
Get the kind of matrix coloring used for the sparse Jacobian computation.
Definition at line 4777 of file CConfig.hpp.
|
inline |
Get the kind of mixing process for averaging quantities at the boundaries.
Definition at line 5209 of file CConfig.hpp.
|
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Get the value of the mixing model for viscosity.
Definition at line 4044 of file CConfig.hpp.
|
inline |
Kind of Multizone Solver.
Definition at line 3905 of file CConfig.hpp.
|
inline |
Get the kind of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.
| [in] | val_obj |
Definition at line 5419 of file CConfig.hpp.
|
inline |
Get the Kind of P1 initialization method applied.
Definition at line 9515 of file CConfig.hpp.
|
inline |
Get the kind of mixing process for averaging quantities at the boundaries.
Definition at line 5132 of file CConfig.hpp.
|
inline |
Static or incremental toggle for POD basis generation type.
Definition at line 9819 of file CConfig.hpp.
|
inline |
Get the Kind of Radiation model applied.
Definition at line 9509 of file CConfig.hpp.
|
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Governing equations of the flow (it can be different from the run time equation).
| [in] | val_zone | - Zone where the soler is applied. |
Definition at line 3912 of file CConfig.hpp.
|
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Get the Kind of Roe Low Dissipation Scheme for Unsteady flows.
Definition at line 9337 of file CConfig.hpp.
|
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Get the kind of sensitivity smoothing technique.
Definition at line 5453 of file CConfig.hpp.
|
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Get the kind of the subgrid scale model.
Definition at line 4530 of file CConfig.hpp.
|
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Get the method for limiting the spatial gradients.
Definition at line 4783 of file CConfig.hpp.
|
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Get the method for limiting the spatial gradients.
Definition at line 4813 of file CConfig.hpp.
|
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Get the method for limiting the spatial gradients.
Definition at line 4807 of file CConfig.hpp.
|
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Get the method for limiting the spatial gradients.
Definition at line 4789 of file CConfig.hpp.
|
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Get the method for limiting the spatial gradients.
Definition at line 4801 of file CConfig.hpp.
|
inline |
Get the method for limiting the spatial gradients.
Definition at line 4795 of file CConfig.hpp.
|
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Governing equations of the flow (it can be different from the run time equation).
| [in] | val_zone | - Zone where the soler is applied. |
Definition at line 3832 of file CConfig.hpp.
|
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Get the kind of integration scheme (explicit or implicit) for the flow equations.
Definition at line 4702 of file CConfig.hpp.
|
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Get the kind of turbomachinery architecture.
Definition at line 5221 of file CConfig.hpp.
|
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Get the kind of the species model.
Definition at line 4524 of file CConfig.hpp.
|
inline |
Get information about the streamwise periodicity (None, Pressure_Drop, Massflow).
Definition at line 6232 of file CConfig.hpp.
|
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Get the kind of SU2 software component.
Definition at line 4470 of file CConfig.hpp.
|
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Get the type of surface motion.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving). |
Definition at line 5953 of file CConfig.hpp.
|
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Get the kind of time integration method.
Definition at line 4539 of file CConfig.hpp.
|
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Get the kind of integration scheme (explicit or implicit) for the adjoint flow equations.
Definition at line 4853 of file CConfig.hpp.
|
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Get the kind of integration scheme (explicit or implicit) for the adjoint turbulence equations.
Definition at line 4939 of file CConfig.hpp.
|
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Get the kind of integration scheme (explicit or implicit) for the flow equations.
Definition at line 4675 of file CConfig.hpp.
|
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Get the kind of integration scheme (explicit or implicit) for the flow equations.
Definition at line 4641 of file CConfig.hpp.
|
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Get the kind of integration scheme (explicit or implicit) for the flow equations.
Definition at line 4657 of file CConfig.hpp.
|
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Get the kind of integration scheme (explicit or implicit) for the radiation equations.
Definition at line 4684 of file CConfig.hpp.
|
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Get the kind of integration scheme (implicit) for the Species equations.
Definition at line 4957 of file CConfig.hpp.
| unsigned short CConfig::GetKind_TimeIntScheme_Template | ( | void | ) |
Get the kind of integration scheme (explicit or implicit) for the template equations.
|
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Get the kind of integration scheme (implicit) for the turbulence equations.
Definition at line 4905 of file CConfig.hpp.
|
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Get the kind of time stepping for the heat equation.
Definition at line 4666 of file CConfig.hpp.
|
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Get the kind of the transition correlations.
Definition at line 4512 of file CConfig.hpp.
|
inline |
Get the kind of the transition model.
Definition at line 4506 of file CConfig.hpp.
|
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Get the transport coefficient model.
Definition at line 3931 of file CConfig.hpp.
|
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Get the kind of the turbulence model.
Definition at line 4500 of file CConfig.hpp.
|
inline |
gets interface kind for an interface marker in turbomachinery problem
Definition at line 5361 of file CConfig.hpp.
|
inline |
Get the kind of turbomachinery architecture.
Definition at line 5215 of file CConfig.hpp.
|
inline |
get marker kind for Turbomachinery performance calculation.
Definition at line 5355 of file CConfig.hpp.
|
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Get kind of upwind scheme for the convective terms.
Definition at line 4566 of file CConfig.hpp.
|
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Get the kind of upwind convective numerical scheme for the adjoint flow equations.
Definition at line 4878 of file CConfig.hpp.
|
inline |
Get the kind of upwind convective numerical scheme for the adjoint turbulence equations.
Definition at line 5021 of file CConfig.hpp.
|
inline |
Get the kind of upwind convective numerical scheme for the flow equations.
Definition at line 4753 of file CConfig.hpp.
|
inline |
Get the kind of upwind convective numerical scheme for the Species equations.
Definition at line 4982 of file CConfig.hpp.
|
inline |
Get the kind of upwind convective numerical scheme for the turbulence equations.
Definition at line 4930 of file CConfig.hpp.
|
inline |
Get the value of the viscosity model.
Definition at line 4038 of file CConfig.hpp.
|
inline |
Get the kind of inlet face interpolation function to use.
Definition at line 9256 of file CConfig.hpp.
|
inline |
Get the kind of inlet face interpolation data type.
Definition at line 9261 of file CConfig.hpp.
|
inline |
Get the interpolation method used for matching between zones.
Definition at line 9221 of file CConfig.hpp.
|
inline |
Get the basis function to use for radial basis function interpolation for FSI.
Definition at line 9231 of file CConfig.hpp.
|
inline |
Get Index of the window function used as weight in the cost functional.
Definition at line 5648 of file CConfig.hpp.
|
inline |
Get the value of the B constant in the Knowles material model.
Definition at line 2296 of file CConfig.hpp.
|
inline |
Get the value of the N constant in the Knowles material model.
Definition at line 2302 of file CConfig.hpp.
|
inline |
Get the temperature polynomial coefficient for thermal conductivity.
| [in] | val_index | - Index of the array with all polynomial coefficients. |
Definition at line 4205 of file CConfig.hpp.
|
inline |
Get the temperature polynomial coefficient for thermal conductivity.
| [in] | val_index | - Index of the array with all polynomial coefficients. |
Definition at line 4212 of file CConfig.hpp.
|
inline |
Get the temperature polynomial coefficients for thermal conductivity.
Definition at line 4218 of file CConfig.hpp.
|
inline |
Get flag for whether a least-squares gradient method is being applied.
TRUE means that a least-squares gradient method is being applied. Definition at line 4268 of file CConfig.hpp.
|
inline |
Get the value of the reference length for non-dimensionalization. This value should always be 1 internally, and is not user-specified.
Definition at line 1826 of file CConfig.hpp.
|
inline |
Get the value of the Reynolds length.
Definition at line 2068 of file CConfig.hpp.
|
inline |
Get the name of the file for libROM to save.
Definition at line 9813 of file CConfig.hpp.
|
inline |
Freeze the value of the limiter after a number of iterations.
Definition at line 2496 of file CConfig.hpp.
|
inline |
Get min error of the linear solver for the implicit formulation.
Definition at line 4293 of file CConfig.hpp.
|
inline |
Get the ILU fill-in level for the linear solver.
Definition at line 4317 of file CConfig.hpp.
|
inline |
Get max number of iterations of the linear solver for the implicit formulation.
Definition at line 4305 of file CConfig.hpp.
|
inline |
Get the number of threads per rank to use for ILU and LU_SGS preconditioners.
Definition at line 9769 of file CConfig.hpp.
|
inline |
Get restart frequency of the linear solver for the implicit formulation.
Definition at line 4323 of file CConfig.hpp.
|
inline |
Get the relaxation factor for iterative linear smoothers.
Definition at line 4329 of file CConfig.hpp.
|
inline |
Get parsed LM option data structure.
Definition at line 9921 of file CConfig.hpp.
| const su2double * CConfig::GetLoad_Dir | ( | const string & | val_index | ) | const |
Get the force direction at a loaded boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 9732 of file CConfig.cpp.
| su2double CConfig::GetLoad_Dir_Multiplier | ( | const string & | val_index | ) | const |
Get the force multiplier at a load boundary in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 9711 of file CConfig.cpp.
| su2double CConfig::GetLoad_Dir_Value | ( | const string & | val_index | ) | const |
Get the force value at a load boundary defined in cartesian coordinates.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 9704 of file CConfig.cpp.
|
inline |
Get the sine load properties.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 9054 of file CConfig.hpp.
| su2double CConfig::GetLoad_Value | ( | const string & | val_index | ) | const |
Get the force value at an load boundary.
| [in] | val_index | - Index corresponding to the load boundary. |
Definition at line 9690 of file CConfig.cpp.
|
inline |
Get the airfoil sections in the slicing process.
| [in] | val_section | - Index of the section. |
Definition at line 3749 of file CConfig.hpp.
|
inline |
Get the name of the variable that we want to retrieve from the lookup table.
Definition at line 2266 of file CConfig.hpp.
|
inline |
Get the value of the Mach number (velocity divided by speed of sound).
Definition at line 1628 of file CConfig.hpp.
|
inline |
Get the mach number based on the mesh velocity and freestream quantities.
Definition at line 5959 of file CConfig.hpp.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 3363 of file CConfig.hpp.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 3371 of file CConfig.hpp.
|
inline |
Get the plotting information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 3644 of file CConfig.hpp.
|
inline |
Get whether marker val_marker is a DEFORM_MESH marker.
| [in] | val_marker | - 0 or 1 depending if the the marker belongs to the DEFORM_MESH subset. |
Definition at line 3721 of file CConfig.hpp.
|
inline |
Get whether marker val_marker is a DEFORM_MESH_SYM_PLANE marker.
| [in] | val_marker | - 0 or 1 depending if the the marker belongs to the DEFORM_MESH_SYM_PLANE subset. |
Definition at line 3728 of file CConfig.hpp.
|
inline |
Get the design information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 3630 of file CConfig.hpp.
|
inline |
Get the DV information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be affected by design variables. |
Definition at line 3700 of file CConfig.hpp.
|
inline |
Get whether marker val_marker is a Fluid_Load marker.
| [in] | val_marker | - 0 or 1 depending if the the marker belongs to the Fluid_Load subset. |
Definition at line 3735 of file CConfig.hpp.
|
inline |
Get the monitoring information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 3623 of file CConfig.hpp.
|
inline |
Get the Giles boundary information for a marker val_marker.
| [in] | val_marker | value of the marker on the grid. |
Definition at line 3679 of file CConfig.hpp.
|
inline |
Get the kind of boundary for each marker.
| [in] | val_marker | - Index of the marker in which we are interested. |
Definition at line 3431 of file CConfig.hpp.
|
inline |
Get the MixingPlane interface information for a marker val_marker.
| [in] | val_marker | value of the marker on the grid. |
Definition at line 3658 of file CConfig.hpp.
|
inline |
Get the monitoring information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 3616 of file CConfig.hpp.
|
inline |
Get the motion information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 3707 of file CConfig.hpp.
|
inline |
Get an internal index that identify the periodic boundary conditions.
| [in] | val_marker | - Value of the marker that correspond with the periodic boundary. |
Definition at line 3609 of file CConfig.hpp.
|
inline |
Get the plotting information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 3637 of file CConfig.hpp.
|
inline |
Get the Python customization for a marker val_marker.
| [in] | val_marker | - Index of the marker in which we are interested. |
Definition at line 3742 of file CConfig.hpp.
|
inline |
Get the send-receive information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 3602 of file CConfig.hpp.
|
inline |
Get the information if gradient treatment uses a marker val_marker.
| [in] | val_marker |
Definition at line 3714 of file CConfig.hpp.
|
inline |
Get the tag if the iMarker defined in the geometry file.
| [in] | val_tag | - Value of the tag in which we are interested. |
Definition at line 3419 of file CConfig.hpp.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 3355 of file CConfig.hpp.
|
inline |
Get the Turbomachinery information for a marker val_marker.
| [in] | val_marker | value of the marker on the grid. |
Definition at line 3665 of file CConfig.hpp.
|
inline |
Get the Turbomachinery flag information for a marker val_marker.
| [in] | val_marker | value of the marker on the grid. |
Definition at line 3672 of file CConfig.hpp.
|
inline |
Get the FSI interface information for a marker val_marker.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 3651 of file CConfig.hpp.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 6891 of file CConfig.hpp.
| unsigned short CConfig::GetMarker_CfgFile_ActDiskOutlet | ( | const string & | val_marker | ) | const |
Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet).
Definition at line 8872 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Analyze | ( | const string & | val_marker | ) | const |
Get the plotting information from the config definition for the marker val_marker.
Definition at line 7951 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Deform_Mesh | ( | const string & | val_marker | ) | const |
Get the DEFORM_MESH information from the config definition for the marker val_marker.
Definition at line 8007 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Deform_Mesh_Sym_Plane | ( | const string & | val_marker | ) | const |
Get the DEFORM_MESH_SYM_PLANE information from the config definition for the marker val_marker.
Definition at line 8014 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Designing | ( | const string & | val_marker | ) | const |
Get the monitoring information from the config definition for the marker val_marker.
Definition at line 7937 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_DV | ( | const string & | val_marker | ) | const |
Get the DV information from the config definition for the marker val_marker.
Definition at line 7993 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_EngineExhaust | ( | const string & | val_marker | ) | const |
Get Actuator Disk Outlet for boundary val_marker (actuator disk inlet).
Definition at line 8888 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Fluid_Load | ( | const string & | val_marker | ) | const |
Get the Fluid_Load information from the config definition for the marker val_marker.
Definition at line 8021 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_GeoEval | ( | const string & | val_marker | ) | const |
Get the monitoring information from the config definition for the marker val_marker.
Definition at line 7930 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Giles | ( | const string & | val_marker | ) | const |
Get the Giles boundary information from the config definition for the marker val_marker.
Definition at line 7986 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_KindBC | ( | const string & | val_marker | ) | const |
Get the boundary information (kind of boundary) in the config information of the marker val_marker.
Definition at line 7916 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_MixingPlaneInterface | ( | const string & | val_marker | ) | const |
Get the MixingPlane interface information from the config definition for the marker val_marker.
Definition at line 7979 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Monitoring | ( | const string & | val_marker | ) | const |
Get the monitoring information from the config definition for the marker val_marker.
Definition at line 7923 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Moving | ( | const string & | val_marker | ) | const |
Get the motion information from the config definition for the marker val_marker.
Definition at line 8000 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_PerBound | ( | const string & | val_marker | ) | const |
Get the periodic information from the config definition of the marker val_marker.
Definition at line 8035 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Plotting | ( | const string & | val_marker | ) | const |
Get the plotting information from the config definition for the marker val_marker.
Definition at line 7944 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_PyCustom | ( | const string & | val_marker | ) | const |
Get the Python customization information from the config definition for the marker val_marker.
Definition at line 8028 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_SobolevBC | ( | const string & | val_marker | ) | const |
Get the gradient boundary information from the config definition for the marker val_marker.
Definition at line 8049 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_TagBound | ( | const string & | val_marker | ) | const |
Get the index in the config information of the marker val_marker.
Definition at line 7900 of file CConfig.cpp.
| string CConfig::GetMarker_CfgFile_TagBound | ( | unsigned short | val_marker | ) | const |
Get the name in the config information of the marker number val_marker.
Definition at line 7912 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_Turbomachinery | ( | const string & | val_marker | ) | const |
Get the TurboPerformance information from the config definition for the marker val_marker.
Definition at line 7965 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_TurbomachineryFlag | ( | const string & | val_marker | ) | const |
Get the TurboPerformance flag information from the config definition for the marker val_marker.
Definition at line 7972 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_CfgFile_ZoneInterface | ( | const string & | val_marker | ) | const |
Get the multi-physics interface information from the config definition for the marker val_marker.
Definition at line 7958 of file CConfig.cpp.
| unsigned short CConfig::GetMarker_Deform_Mesh | ( | const string & | val_marker | ) | const |
Get the internal index for a DEFORM_MESH boundary val_marker.
Definition at line 8941 of file CConfig.cpp.
|
inline |
Get a bool for whether the marker is deformed. val_marker.
| [in] | val_marker | - Name of the marker to test. |
Definition at line 6828 of file CConfig.hpp.
| unsigned short CConfig::GetMarker_Deform_Mesh_Sym_Plane | ( | const string & | val_marker | ) | const |
Get the internal index for a DEFORM_MESH_SYM_PLANE boundary val_marker.
Definition at line 8951 of file CConfig.cpp.
|
inline |
Get the name of the DEFORM_MESH_SYM_PLANE boundary defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 6867 of file CConfig.hpp.
|
inline |
Get the name of the DEFORM_MESH boundary defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 6859 of file CConfig.hpp.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 3395 of file CConfig.hpp.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 3387 of file CConfig.hpp.
| unsigned short CConfig::GetMarker_Fluid_Load | ( | const string & | val_marker | ) | const |
Get the internal index for a Fluid_Load boundary val_marker.
Definition at line 8961 of file CConfig.cpp.
|
inline |
Get the name of the Fluid_Load boundary defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 6875 of file CConfig.hpp.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 3411 of file CConfig.hpp.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 3403 of file CConfig.hpp.
| unsigned short CConfig::GetMarker_Moving | ( | const string & | val_marker | ) | const |
Get the internal index for a moving boundary val_marker.
Definition at line 8931 of file CConfig.cpp.
|
inline |
Get a bool for whether a marker is moving. val_marker.
| [in] | val_marker | - Name of the marker to test. |
Definition at line 6807 of file CConfig.hpp.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 6851 of file CConfig.hpp.
|
inline |
Get the number of FSI interface markers val_marker.
| [in] | void. |
Definition at line 3686 of file CConfig.hpp.
|
inline |
Get the index of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 3379 of file CConfig.hpp.
|
inline |
get outlet bounds name for Turbomachinery performance calculation.
Definition at line 5367 of file CConfig.hpp.
| unsigned short CConfig::GetMarker_Periodic_Donor | ( | const string & | val_marker | ) | const |
Get the rotationally periodic donor marker for boundary val_marker.
Definition at line 8705 of file CConfig.cpp.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 6883 of file CConfig.hpp.
|
inline |
Get the marker shroud.
Definition at line 5293 of file CConfig.hpp.
| unsigned short CConfig::GetMarker_SobolevBC | ( | const string & | val_marker | ) | const |
Get the internal index for a gradient boundary condition val_marker.
Definition at line 8971 of file CConfig.cpp.
| bool CConfig::GetMarker_StrongBC | ( | const string & | val_index | ) | const |
Get if boundary is strong or weak.
| [in] | val_index | - Index corresponding to the boundary. |
Definition at line 9753 of file CConfig.cpp.
|
inline |
get inlet bounds name for Turbomachinery performance calculation.
Definition at line 5343 of file CConfig.hpp.
|
inline |
get outlet bounds name for Turbomachinery performance calculation.
Definition at line 5349 of file CConfig.hpp.
| unsigned short CConfig::GetMarker_ZoneInterface | ( | const string & | val_marker | ) | const |
Get the name of the marker val_marker.
Definition at line 8042 of file CConfig.cpp.
|
inline |
Get the mesh motion origin.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) |
| [in] | iDim | - spatial component |
Definition at line 5981 of file CConfig.hpp.
|
inline |
Get pitching amplitude of the marker.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) |
| [in] | iDim | - spatial component |
Definition at line 6084 of file CConfig.hpp.
|
inline |
Get pitching rate of the marker.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) |
| [in] | iDim | - spatial component |
Definition at line 6069 of file CConfig.hpp.
|
inline |
Get pitching phase of the marker.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) \ |
| [in] | iDim | - spatial component |
Definition at line 6099 of file CConfig.hpp.
|
inline |
Get plunging amplitude of the marker.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) |
| [in] | iDim | - spatial component |
Definition at line 6129 of file CConfig.hpp.
|
inline |
Get plunging rate of the marker.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) |
| [in] | iDim | - spatial component |
Definition at line 6114 of file CConfig.hpp.
|
inline |
Get the rotation rate of the marker.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) |
| [in] | iDim | - spatial component |
Definition at line 6044 of file CConfig.hpp.
|
inline |
Get the name of the marker val_iMarker.
Definition at line 6490 of file CConfig.hpp.
|
inline |
Get the translational velocity of the marker.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) |
| [in] | iDim | - spatial component |
Definition at line 6012 of file CConfig.hpp.
|
inline |
Compressibility/incompressibility of the solids analysed using the structural solver.
Definition at line 2396 of file CConfig.hpp.
|
inline |
Get the Material Density.
Definition at line 2390 of file CConfig.hpp.
|
inline |
Compressibility/incompressibility of the solids analysed using the structural solver.
Definition at line 2402 of file CConfig.hpp.
|
inline |
Get maximum number of POD basis dimensions (default: 100).
Definition at line 9825 of file CConfig.hpp.
|
inline |
Get the Courant Friedrich Levi number for unsteady simulations.
Definition at line 2922 of file CConfig.hpp.
|
inline |
Get the maximum simulation time for time-domain problems.
Definition at line 9485 of file CConfig.hpp.
|
inline |
Get the maximum velocity^2 in the domain for the incompressible preconditioner.
Definition at line 9313 of file CConfig.hpp.
|
inline |
Get the minimum value of Beta for Roe-Turkel preconditioner.
Definition at line 6172 of file CConfig.hpp.
|
inline |
Get the format of the input/output grid.
Definition at line 5611 of file CConfig.hpp.
|
inline |
Get name of the input grid.
Definition at line 5584 of file CConfig.hpp.
|
inline |
Get name of the output grid, this parameter is important for grid adaptation and deformation.
Definition at line 5591 of file CConfig.hpp.
|
inline |
Get the length of the analytic RECTANGLE or BOX grid in the specified coordinate direction.
Definition at line 9589 of file CConfig.hpp.
|
inline |
Get the offset from 0.0 of the analytic RECTANGLE or BOX grid in the specified coordinate direction.
Definition at line 9595 of file CConfig.hpp.
|
inline |
Get the number of grid points in the analytic RECTANGLE or BOX grid in the specified coordinate direction.
Definition at line 9583 of file CConfig.hpp.
|
inline |
Get the number of implicit Jacobi smoothings of the correction in a multigrid strategy.
| [in] | val_mesh | - Index of the grid. |
Definition at line 3783 of file CConfig.hpp.
|
inline |
Get the number of post-smoothings in a multigrid strategy.
| [in] | val_mesh | - Index of the grid. |
Definition at line 3773 of file CConfig.hpp.
|
inline |
Get the number of pre-smoothings in a multigrid strategy.
| [in] | val_mesh | - Index of the grid. |
Definition at line 3763 of file CConfig.hpp.
|
inline |
Get the kind of multigrid (V or W).
Definition at line 2884 of file CConfig.hpp.
|
inline |
Value of the minimum residual value (log10 scale).
Definition at line 6548 of file CConfig.hpp.
|
inline |
Get the minimum value of Beta for Roe-Turkel preconditioner.
Definition at line 6166 of file CConfig.hpp.
|
inline |
Get mixedout coefficients.
Definition at line 5191 of file CConfig.hpp.
|
inline |
Get the magnitude of the free-stream velocity of the fluid.
Definition at line 1765 of file CConfig.hpp.
|
inline |
Get the non-dimensional magnitude of the free-stream velocity of the fluid.
Definition at line 1771 of file CConfig.hpp.
|
inline |
Get the value of the molecular weight for an incompressible ideal gas (g/mol).
Definition at line 1694 of file CConfig.hpp.
|
inline |
Get final Outlet Pressure value for the ramp.
Definition at line 5174 of file CConfig.hpp.
|
inline |
Indicates if mixture is monoatomic.
Definition at line 5555 of file CConfig.hpp.
|
inline |
Get the mesh motion origin.
| [in] | iDim | - spatial component |
Definition at line 5966 of file CConfig.hpp.
|
inline |
Get if we should update the motion origin.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 6160 of file CConfig.hpp.
| SU2_MPI::Comm CConfig::GetMPICommunicator | ( | ) | const |
Get the MPI communicator of SU2.
Definition at line 258 of file CConfig.cpp.
|
inline |
Get the value of the constant viscosity.
Definition at line 4068 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensional constant viscosity.
Definition at line 4074 of file CConfig.hpp.
|
inline |
Get the temperature polynomial coefficient for viscosity.
| [in] | val_index | - Index of the array with all polynomial coefficients. |
Definition at line 4185 of file CConfig.hpp.
|
inline |
Get the temperature polynomial coefficient for viscosity.
| [in] | val_index | - Index of the array with all polynomial coefficients. |
Definition at line 4192 of file CConfig.hpp.
|
inline |
Get the temperature polynomial coefficients for viscosity.
Definition at line 4198 of file CConfig.hpp.
|
inline |
Get the value of the reference viscosity for Sutherland model.
Definition at line 4126 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensional reference viscosity for Sutherland model.
Definition at line 4132 of file CConfig.hpp.
|
inline |
Get the value of the reference S for Sutherland model.
Definition at line 4152 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensional reference S for Sutherland model.
Definition at line 4158 of file CConfig.hpp.
|
inline |
Get the value of the reference temperature for Sutherland model.
Definition at line 4138 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensional reference temperature for Sutherland model.
Definition at line 4144 of file CConfig.hpp.
| string CConfig::GetMultiInstance_FileName | ( | string | val_filename, |
| int | val_iInst, | ||
| const string & | ext | ||
| ) | const |
Append the instance index to the restart or the solution files.
| [in] | val_filename | - the base filename. |
| [in] | val_iInst | - the current instance. |
| [in] | ext | - the filename extension. |
Definition at line 8427 of file CConfig.cpp.
| string CConfig::GetMultiInstance_HistoryFileName | ( | string | val_filename, |
| int | val_iInst | ||
| ) | const |
Append the instance index to the restart or the solution files.
| [in] | val_filename | - the base filename. |
| [in] | val_iInst | - the current instance. |
Definition at line 8440 of file CConfig.cpp.
| string CConfig::GetMultizone_FileName | ( | string | val_filename, |
| int | val_iZone, | ||
| const string & | ext | ||
| ) | const |
Append the zone index to the restart or the solution files.
Definition at line 8396 of file CConfig.cpp.
| string CConfig::GetMultizone_HistoryFileName | ( | string | val_filename, |
| int | val_iZone, | ||
| const string & | ext | ||
| ) | const |
Append the zone index to the restart or the solution files.
| [in] | val_filename | - the base filename. |
| [in] | val_iZone | - the zone ID. |
| [in] | ext | - the filename extension. |
Definition at line 8413 of file CConfig.cpp.
|
inline |
Check if the mesh read supports multiple zones.
Definition at line 9497 of file CConfig.hpp.
|
inline |
Get whether the simulation we are running is a multizone simulation.
Definition at line 9127 of file CConfig.hpp.
|
inline |
Check if the mesh read supports multiple zones.
Definition at line 9503 of file CConfig.hpp.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 4575 of file CConfig.hpp.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 4617 of file CConfig.hpp.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 4626 of file CConfig.hpp.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 4584 of file CConfig.hpp.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 4593 of file CConfig.hpp.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 4608 of file CConfig.hpp.
|
inline |
Get if the upwind scheme used MUSCL or not.
Definition at line 4602 of file CConfig.hpp.
|
inline |
Get the defintion of the nacelle location.
| [in] | val_index | - Index of the section. |
Definition at line 3756 of file CConfig.hpp.
|
inline |
number Turbomachinery blades computed using the pitch information.
Definition at line 5257 of file CConfig.hpp.
|
inline |
Get the number of config files.
Definition at line 9437 of file CConfig.hpp.
|
inline |
Get the number of control variables for flamelet model.
Definition at line 2212 of file CConfig.hpp.
|
inline |
Get the number of convergence monitoring fields for inner convergence monitoring. return Number of convergence monitoring fields.
Definition at line 9677 of file CConfig.hpp.
|
inline |
Get number of listed look-up table or multi-layer perceptron input files.
Definition at line 3974 of file CConfig.hpp.
|
static |
Gets the number of dimensions in the mesh file.
| [in] | val_mesh_filename | - Name of the file with the grid information. |
| [in] | val_format | - Format of the file with the grid information. |
Definition at line 712 of file CConfig.cpp.
|
inline |
Get the dimensionality of the electric field.
Definition at line 9002 of file CConfig.hpp.
|
inline |
Get the number of design variables.
Definition at line 2966 of file CConfig.hpp.
|
inline |
Get the total number of design variables.
Definition at line 2980 of file CConfig.hpp.
|
inline |
Get the number of design variables.
Definition at line 2972 of file CConfig.hpp.
|
inline |
Get the number of different materials for the elasticity solver.
Definition at line 8983 of file CConfig.hpp.
|
inline |
Get the number of different electric constants.
Definition at line 2284 of file CConfig.hpp.
|
inline |
Get the number of different values for the modulus of the electric field.
Definition at line 8996 of file CConfig.hpp.
|
inline |
Return true if a NEMO solver is in use.
Definition at line 3880 of file CConfig.hpp.
|
inline |
Get Newmark alpha parameter.
Definition at line 8965 of file CConfig.hpp.
|
inline |
Get Newmark delta parameter.
Definition at line 8971 of file CConfig.hpp.
|
inline |
Get whether to use a Newton-Krylov method.
Definition at line 4355 of file CConfig.hpp.
|
inline |
Get Newton-Krylov floating-point parameters.
Definition at line 4365 of file CConfig.hpp.
|
inline |
Get Newton-Krylov integer parameters.
Definition at line 4360 of file CConfig.hpp.
|
inline |
Get the number of planes to fix in the I direction.
Definition at line 3813 of file CConfig.hpp.
|
inline |
Get the number of planes to fix in the J direction.
Definition at line 3819 of file CConfig.hpp.
|
inline |
Get the number of planes to fix in the K direction.
Definition at line 3825 of file CConfig.hpp.
|
inline |
Get the number of iterations to evaluate the parametric coordinates.
Definition at line 8659 of file CConfig.hpp.
|
inline |
Get the number of FFD boxes.
Definition at line 2993 of file CConfig.hpp.
|
inline |
Get the number of history output variables requested.
Definition at line 9610 of file CConfig.hpp.
|
inline |
Get the ID for the FEA region that we want to compute the gradient for using direct differentiation.
Definition at line 9133 of file CConfig.hpp.
|
inline |
Get the total number of types in Kind_Inc_Inlet list.
Definition at line 5096 of file CConfig.hpp.
|
inline |
Get the number of inner iterations.
Definition at line 9449 of file CConfig.hpp.
|
inline |
Get the number of integration coefficients provided by the user.
Definition at line 8977 of file CConfig.hpp.
|
inline |
Get the number of subiterations while a ramp is applied.
Definition at line 8911 of file CConfig.hpp.
|
inline |
Get the number of time levels for time accurate local time stepping.
Definition at line 3029 of file CConfig.hpp.
|
inline |
Get the number of sections.
Definition at line 5390 of file CConfig.hpp.
|
inline |
Get the number of transported scalars for combustion.
Definition at line 2261 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers.
Definition at line 3137 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers.
Definition at line 3143 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers of the local process including send/receive domains.
Definition at line 3071 of file CConfig.hpp.
|
inline |
Get the total number of moving markers.
Definition at line 3185 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers in the config file.
Definition at line 3077 of file CConfig.hpp.
|
inline |
Get the total number of deformable markers at the boundary.
Definition at line 3119 of file CConfig.hpp.
|
inline |
Get the total number of DV markers.
Definition at line 3161 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers.
Definition at line 3107 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers.
Definition at line 3101 of file CConfig.hpp.
|
inline |
Get the number of Euler boundary markers.
Definition at line 3083 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers.
Definition at line 3131 of file CConfig.hpp.
|
inline |
Get the total number of markers in which the flow load is computed/employed.
Definition at line 3125 of file CConfig.hpp.
|
inline |
Get the total (local) number of heat flux markers.
Definition at line 3197 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers in the cfg plus the possible send/receive domains.
Definition at line 3095 of file CConfig.hpp.
|
inline |
number mixing plane interface specified from config file.
Definition at line 5245 of file CConfig.hpp.
|
inline |
Get the total number of monitoring markers.
Definition at line 3155 of file CConfig.hpp.
|
inline |
Get the total number of moving markers.
Definition at line 3167 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers.
Definition at line 3113 of file CConfig.hpp.
|
inline |
Get the total number of boundary markers.
Definition at line 3149 of file CConfig.hpp.
|
inline |
Get the total number of periodic markers.
Definition at line 3191 of file CConfig.hpp.
|
inline |
Get the total number of Python customizable markers.
Definition at line 3179 of file CConfig.hpp.
|
inline |
Get number of shroud markers.
Definition at line 5287 of file CConfig.hpp.
|
inline |
Get the total number of markers for gradient treatment.
Definition at line 3173 of file CConfig.hpp.
|
inline |
Get the number of symmetry boundary markers.
Definition at line 3089 of file CConfig.hpp.
|
inline |
number Turbomachinery performance option specified from config file.
Definition at line 5281 of file CConfig.hpp.
|
inline |
number Turbomachinery performance option specified from config file.
Definition at line 5299 of file CConfig.hpp.
|
inline |
Get the number of markers in the multizone interface.
Definition at line 6496 of file CConfig.hpp.
|
inline |
Get the number of multigrid levels.
Definition at line 2859 of file CConfig.hpp.
|
inline |
Get the total number of objectives in kind_objective list.
Definition at line 3209 of file CConfig.hpp.
|
inline |
Get the current number of non-physical nodes in the solution.
Definition at line 8817 of file CConfig.hpp.
|
inline |
Get the current number of non-physical reconstructions for 2nd-order upwinding.
Definition at line 8829 of file CConfig.hpp.
|
inline |
Get the number of outer iterations.
Definition at line 9455 of file CConfig.hpp.
|
inline |
Get the number of coefficients in the temperature polynomial models.
Definition at line 4164 of file CConfig.hpp.
|
inline |
Get the number of samples used in quasi-Newton methods.
Definition at line 4345 of file CConfig.hpp.
|
inline |
Get the number of Runge-Kutta steps.
Definition at line 3023 of file CConfig.hpp.
|
inline |
Get the total number of rough markers.
Definition at line 3203 of file CConfig.hpp.
|
inline |
Get the number of total transported scalars for flamelet model.
Definition at line 2217 of file CConfig.hpp.
|
inline |
Get the number of screen output variables requested (maximum 6)
Definition at line 9600 of file CConfig.hpp.
|
inline |
get number span-wise sections to compute 3D BC and performance for turbomachinery.
Definition at line 5332 of file CConfig.hpp.
|
inline |
number span-wise sections to compute performance for turbomachinery.
Definition at line 5322 of file CConfig.hpp.
|
inline |
number span-wise sections to compute 3D BC and performance for turbomachinery.
Definition at line 5311 of file CConfig.hpp.
|
inline |
Provides the number of species present in the gas mixture.
Definition at line 5467 of file CConfig.hpp.
|
inline |
Get the number of time iterations.
Definition at line 9461 of file CConfig.hpp.
|
inline |
Get the number time DOFs for ADER-DG.
Definition at line 3041 of file CConfig.hpp.
|
inline |
Retrieves the number of periodic time instances for Harmonic Balance.
Definition at line 3233 of file CConfig.hpp.
|
inline |
Get the number time integration points for ADER-DG.
Definition at line 3053 of file CConfig.hpp.
|
inline |
Get the number of Turbulence Variables.
Definition at line 4494 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized engine turbulence intensity.
Definition at line 2038 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream turbulence intensity.
Definition at line 2020 of file CConfig.hpp.
|
inline |
Get the number of increments for an incremental load.
Definition at line 9145 of file CConfig.hpp.
|
inline |
Get the number of donor points to use in Nearest Neighbor interpolation.
Definition at line 9251 of file CConfig.hpp.
|
inline |
Get the number of user scalars for flamelet model.
Definition at line 2222 of file CConfig.hpp.
| unsigned short CConfig::GetnVar | ( | void | ) |
Provides the number of varaibles.
|
inline |
Get the number of history output variables requested.
Definition at line 9620 of file CConfig.hpp.
|
inline |
GetnVolumeOutputFiles.
Definition at line 9726 of file CConfig.hpp.
|
inline |
Get the total number of heat flux markers.
Definition at line 3937 of file CConfig.hpp.
|
inline |
Get the number of sections for computing internal volume.
Definition at line 5396 of file CConfig.hpp.
|
inline |
Get the number of convergence monitoring fields for time convergence monitoring. return Number of convergence monitoring fields.
Definition at line 9671 of file CConfig.hpp.
|
static |
Gets the number of zones in the mesh file.
| [in] | val_mesh_filename | - Name of the file with the grid information. |
| [in] | val_format | - Format of the file with the grid information. |
Definition at line 590 of file CConfig.cpp.
|
inline |
Provides the number of varaibles.
Definition at line 5521 of file CConfig.hpp.
| string CConfig::GetObjFunc_Extension | ( | string | val_filename | ) | const |
Append the input filename string with the appropriate objective function extension.
| [in] | val_filename | - String value of the base filename. |
Definition at line 8453 of file CConfig.cpp.
|
inline |
Get the name of the file with the gradient of the objective function.
Definition at line 5734 of file CConfig.hpp.
|
inline |
Get the name of the file with the hessian of the objective function.
Definition at line 9879 of file CConfig.hpp.
|
inline |
Get the name of the file with the gradient of the objective function.
Definition at line 5740 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 1996 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 1984 of file CConfig.hpp.
|
inline |
Get the Harmonic Balance frequency pointer.
Definition at line 6147 of file CConfig.hpp.
|
inline |
Get the value of the reference angular velocity for non-dimensionalization.
Definition at line 1898 of file CConfig.hpp.
|
inline |
Get the w constant factor define a lower limit by multiplication with values in SST turbulencemodel.
Definition at line 2032 of file CConfig.hpp.
|
inline |
Get the bound for the line search.
Definition at line 8698 of file CConfig.hpp.
|
inline |
Get the scale factor for the line search.
Definition at line 8692 of file CConfig.hpp.
|
inline |
Get the current FSI iteration number.
Definition at line 3281 of file CConfig.hpp.
| su2double CConfig::GetOutlet_Area | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8865 of file CConfig.cpp.
| su2double CConfig::GetOutlet_Density | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8858 of file CConfig.cpp.
| su2double CConfig::GetOutlet_MassFlow | ( | const string & | val_marker | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8851 of file CConfig.cpp.
| su2double CConfig::GetOutlet_Pressure | ( | const string & | val_index | ) | const |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9076 of file CConfig.cpp.
|
inline |
Get the output precision to be used in <ofstream>.precision(value) for history and SU2_DOT output.
Definition at line 5623 of file CConfig.hpp.
|
inline |
Get a parameter of the particular design variable.
| [in] | val_dv | - Number of the design variable that we want to read. |
| [in] | val_param | - Index of the parameter that we want to read. |
Definition at line 2930 of file CConfig.hpp.
|
inline |
Get the ParMETIS load balancing weight for edges.
Definition at line 9794 of file CConfig.hpp.
|
inline |
Get the ParMETIS load balancing weight for points.
Definition at line 9789 of file CConfig.hpp.
|
inline |
Get the ParMETIS load balancing tolerance.
Definition at line 9784 of file CConfig.hpp.
|
inline |
Get the desired factorization frequency for PaStiX.
Definition at line 9738 of file CConfig.hpp.
|
inline |
Get the desired level of fill for the PaStiX ILU.
Definition at line 9750 of file CConfig.hpp.
|
inline |
Get the desired level of verbosity for PaStiX.
Definition at line 9744 of file CConfig.hpp.
|
inline |
Get the translation vector for a periodic transformation.
| [in] | val_index | - Index corresponding to the periodic transformation. |
Definition at line 6691 of file CConfig.hpp.
| const su2double * CConfig::GetPeriodicRotAngles | ( | const string & | val_marker | ) | const |
Angles of rotation for a rotational periodic boundary.
Definition at line 8691 of file CConfig.cpp.
| const su2double * CConfig::GetPeriodicRotCenter | ( | const string & | val_marker | ) | const |
Center of rotation for a rotational periodic boundary.
Definition at line 8684 of file CConfig.cpp.
| const su2double * CConfig::GetPeriodicTranslation | ( | const string & | val_marker | ) | const |
Translation vector for a translational periodic boundary.
Definition at line 8698 of file CConfig.cpp.
|
inline |
Get the current physical time.
Definition at line 3299 of file CConfig.hpp.
|
inline |
Get the pitching amplitude of the mesh.
| [in] | iDim | - spatial component |
Definition at line 6076 of file CConfig.hpp.
|
inline |
Get the pitching rate of the mesh.
| [in] | iDim | - spatial component |
Definition at line 6061 of file CConfig.hpp.
|
inline |
Get the pitching phase of the mesh.
| [in] | iDim | - spatial component. |
Definition at line 6091 of file CConfig.hpp.
|
inline |
Get index of the upper and lower horizontal plane.
| [in] | index | - 0 means upper surface, and 1 means lower surface. |
Definition at line 1561 of file CConfig.hpp.
|
inline |
Get information about writing sectional force files.
TRUE means that sectional force files will be written for specified markers. Definition at line 3340 of file CConfig.hpp.
|
inline |
Get the plunging amplitude of the mesh.
| [in] | iDim | - spatial component |
Definition at line 6121 of file CConfig.hpp.
|
inline |
Get the plunging rate of the mesh.
| [in] | iDim | - spatial component |
Definition at line 6106 of file CConfig.hpp.
|
inline |
Get the p-norm for heat-flux objective functions (adjoint problem).
Definition at line 1718 of file CConfig.hpp.
|
inline |
Get the Poisson's ratio.
Definition at line 2384 of file CConfig.hpp.
|
inline |
Get information about the poisson solver condition.
TRUE if it is a poisson solver condition; otherwise FALSE. Definition at line 6202 of file CConfig.hpp.
|
inline |
Value of the position of the Near Field (y coordinate for 2D, and z coordinate for 3D).
Definition at line 6584 of file CConfig.hpp.
|
inline |
Get the value of the laminar Prandtl number.
Definition at line 1777 of file CConfig.hpp.
|
inline |
Get the value of the turbulent Prandtl number.
Definition at line 1783 of file CConfig.hpp.
|
inline |
Get whether a predictor is used for FSI applications.
Definition at line 9085 of file CConfig.hpp.
|
inline |
Get the order of the predictor for FSI applications.
Definition at line 9091 of file CConfig.hpp.
|
inline |
Preferential diffusion combustion problem.
Definition at line 2202 of file CConfig.hpp.
|
inline |
Get the value of the critical pressure.
Definition at line 4020 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream pressure.
Definition at line 1910 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream pressure.
Definition at line 1916 of file CConfig.hpp.
|
inline |
Get the value of the reference pressure for non-dimensionalization.
Definition at line 1832 of file CConfig.hpp.
|
inline |
Get the value of the thermodynamic pressure.
Definition at line 1922 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized thermodynamic pressure.
Definition at line 1928 of file CConfig.hpp.
| su2double CConfig::GetPressureOut_BC | ( | ) | const |
Get the outlet pressure imposed as BC for internal flow.
Definition at line 9167 of file CConfig.cpp.
|
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Decide whether it's necessary to read a reference geometry.
TRUE if it's necessary to read a reference geometry, FALSE otherwise. Definition at line 2360 of file CConfig.hpp.
|
inline |
Get the name of the file with the reference geometry of the structural problem.
Definition at line 2378 of file CConfig.hpp.
|
inline |
Get whether to print inlet interpolated data or not.
Definition at line 9266 of file CConfig.hpp.
|
inline |
Identifies if the mesh is matching or not (temporary, while implementing interpolation procedures).
TRUE if the mesh is matching, FALSE otherwise. Definition at line 8941 of file CConfig.hpp.
|
inline |
Get the factor applied during quadrature of curved elements.
Definition at line 9176 of file CConfig.hpp.
|
inline |
Get the factor applied during quadrature of straight elements.
Definition at line 9170 of file CConfig.hpp.
|
inline |
Get the factor applied during time quadrature for ADER-DG.
Definition at line 9182 of file CConfig.hpp.
|
inline |
Get the basis function radius to use for radial basis function interpolation for FSI.
Definition at line 9241 of file CConfig.hpp.
|
inline |
Get option of whether to use polynomial terms in Radial Basis Function interpolation.
Definition at line 9236 of file CConfig.hpp.
|
inline |
Get the tolerance used to prune the interpolation matrix (making it sparser).
Definition at line 9246 of file CConfig.hpp.
|
inline |
Check if the user wants to apply the load as a ramp.
TRUE means that the load is to be applied as a ramp. Definition at line 9029 of file CConfig.hpp.
|
inline |
Get the maximum time of the ramp.
Definition at line 9035 of file CConfig.hpp.
|
inline |
Check if the user wants to apply the load as a ramp.
TRUE means that the load is to be applied as a ramp. Definition at line 9041 of file CConfig.hpp.
|
inline |
Get Outlet Pressure Ramp option.
Definition at line 5185 of file CConfig.hpp.
|
inline |
Get coeff for Outlet Pressure Ramp.
Definition at line 5162 of file CConfig.hpp.
|
inline |
Get Rotating Frame Ramp option.
Definition at line 5156 of file CConfig.hpp.
|
inline |
Get coeff for Rotating Frame Ramp.
Definition at line 5150 of file CConfig.hpp.
|
inline |
Flag for whether binary SU2 native restart files are read.
TRUE then the code will load binary restart files. Definition at line 5491 of file CConfig.hpp.
|
inline |
Get flag for whether a second gradient calculation is required for upwind reconstruction alone.
TRUE means that a second gradient will be calculated for upwind reconstruction. Definition at line 4262 of file CConfig.hpp.
|
inline |
Get the kind of incompressible non-dimensionalization.
Definition at line 4482 of file CConfig.hpp.
|
inline |
Get the kind of non-dimensionalization.
Definition at line 4476 of file CConfig.hpp.
|
inline |
Get the reference area for non dimensional coefficient computation. If the value from the is 0 then, the code will compute the reference area using the projection of the shape into the z plane (3D) or the x plane (2D).
Definition at line 2076 of file CConfig.hpp.
|
inline |
Get the reference element length for computing the slope limiting epsilon.
Definition at line 2420 of file CConfig.hpp.
|
inline |
Decide whether it's necessary to read a reference geometry.
Definition at line 2331 of file CConfig.hpp.
|
inline |
Get the name of the file with the reference geometry of the structural problem.
Definition at line 2342 of file CConfig.hpp.
|
inline |
Get the format of the reference geometry file.
Definition at line 2348 of file CConfig.hpp.
|
inline |
Get the penalty weight value for the objective function.
Definition at line 9068 of file CConfig.hpp.
|
inline |
Consider only the surface of the reference geometry.
Definition at line 2336 of file CConfig.hpp.
|
inline |
Get the reference length for computing moment (the default value is 1).
Definition at line 2414 of file CConfig.hpp.
|
inline |
Get the values for the reference node displacement.
| [in] | val_coeff | - Index of the displacement. |
Definition at line 2320 of file CConfig.hpp.
|
inline |
Get the ID of the reference node.
Definition at line 2314 of file CConfig.hpp.
|
inline |
Get the penalty weight value for the objective function.
Definition at line 2326 of file CConfig.hpp.
|
inline |
Get reference origin for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 1504 of file CConfig.hpp.
|
inline |
Get reference origin x-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 1519 of file CConfig.hpp.
|
inline |
Get reference origin y-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 1526 of file CConfig.hpp.
|
inline |
Get reference origin z-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
Definition at line 1533 of file CConfig.hpp.
|
inline |
Get the reference coefficient for detecting sharp edges.
Definition at line 2426 of file CConfig.hpp.
|
inline |
Get whether a relaxation parameter is used for FSI applications.
Definition at line 9109 of file CConfig.hpp.
|
inline |
Get Newton solver relaxation factor for data-driven fluid models.
Definition at line 3980 of file CConfig.hpp.
|
inline |
Get the relaxation factor for solution updates of adjoint solvers.
Definition at line 4334 of file CConfig.hpp.
|
inline |
Get the relaxation coefficient of the CHT coupling.
Definition at line 4340 of file CConfig.hpp.
|
inline |
Get the relaxation method chosen for the simulation.
Definition at line 9157 of file CConfig.hpp.
|
inline |
Get information about element reorientation.
TRUE means that elements can be reoriented if suspected unhealthy Definition at line 2916 of file CConfig.hpp.
|
inline |
Get functional that is going to be used to evaluate the residual flow convergence.
Definition at line 5786 of file CConfig.hpp.
|
inline |
Provides the restart information.
TRUE then the code will use the solution as restart. Definition at line 5485 of file CConfig.hpp.
|
inline |
Get the name of the restart file for the adjoint variables (drag objective function).
Definition at line 5722 of file CConfig.hpp.
|
inline |
Set the sum of the bandwidth for writing binary restarts (to be averaged later).
Definition at line 9325 of file CConfig.hpp.
|
inline |
Get the name of the restart file for the flow variables.
Definition at line 5716 of file CConfig.hpp.
|
inline |
For some problems like adjoint or the linearized equations it is necessary to restart the flow solution.
TRUE then the code will restart the flow solution. Definition at line 5535 of file CConfig.hpp.
|
inline |
Get the restart iteration.
Definition at line 9473 of file CConfig.hpp.
|
inline |
Get the value of the freestream momentum thickness Reynolds number.
Definition at line 2008 of file CConfig.hpp.
|
inline |
Get the Reynolds number. Dimensionless number that gives a measure of the ratio of inertial forces to viscous forces and consequently quantifies the relative importance of these two types of forces for given flow condition.
Definition at line 2510 of file CConfig.hpp.
| const su2double * CConfig::GetRiemann_FlowDir | ( | const string & | val_marker | ) | const |
Get the Flowdir at Riemann boundary.
| [in] | val_marker | - Index corresponding to the Riemann boundary. |
Definition at line 9104 of file CConfig.cpp.
|
inline |
Get the kind of Riemann solver for the DG method (FEM flow solver).
Definition at line 9164 of file CConfig.hpp.
| su2double CConfig::GetRiemann_Var1 | ( | const string & | val_marker | ) | const |
Get the var 1 at Riemann boundary.
| [in] | val_marker | - Index corresponding to the Riemann boundary. |
Definition at line 9090 of file CConfig.cpp.
| su2double CConfig::GetRiemann_Var2 | ( | const string & | val_marker | ) | const |
Get the var 2 at Riemann boundary.
| [in] | val_marker | - Index corresponding to the Riemann boundary. |
Definition at line 9097 of file CConfig.cpp.
|
inline |
Returns the Roe kappa (multipler of the dissipation term).
Definition at line 4370 of file CConfig.hpp.
|
inline |
Get frequency of unsteady time steps to save (default: 1).
Definition at line 9831 of file CConfig.hpp.
|
inline |
Get information about the rotational frame.
TRUE if there is a rotational frame; otherwise FALSE. Definition at line 6313 of file CConfig.hpp.
|
inline |
Get the rotation rate of the mesh.
| [in] | iDim | - spatial component |
Definition at line 6028 of file CConfig.hpp.
|
inline |
Get parsed SA option data structure.
Definition at line 9915 of file CConfig.hpp.
|
inline |
Get whether or not to save solution data to libROM.
Definition at line 9807 of file CConfig.hpp.
|
inline |
Get the value of the scattering coefficient of the medium.
Definition at line 9527 of file CConfig.hpp.
|
inline |
Get the value of the laminar Schmidt number for scalar transport.
Definition at line 4108 of file CConfig.hpp.
|
inline |
Get the value of the turbulent Schmidt number for scalar transport.
Definition at line 4114 of file CConfig.hpp.
|
inline |
GetScreen_Wrt_Freq_Inner.
| [in] | iter | index for Time (0), Outer (1), or Inner (2) iterations |
Definition at line 9709 of file CConfig.hpp.
|
inline |
Get the screen output field iField.
Definition at line 9605 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized actuator disk turbulence intensity.
Definition at line 2044 of file CConfig.hpp.
|
inline |
Get the wing semi span.
Definition at line 4376 of file CConfig.hpp.
|
inline |
Provides information about if the sharp edges are going to be removed from the sensitivity.
FALSE means that the sharp edges will be removed from the sensitivity. Definition at line 5054 of file CConfig.hpp.
|
inline |
Get information about the format for the input volume sensitvities.
Definition at line 3334 of file CConfig.hpp.
|
inline |
Get exponent for density-based stiffness penalization.
Definition at line 9393 of file CConfig.hpp.
|
inline |
Get lower bound for density-based stiffness penalization.
Definition at line 9398 of file CConfig.hpp.
|
inline |
Check if the user wants to apply the load as a ramp.
TRUE means that the load is to be applied as a ramp. Definition at line 9047 of file CConfig.hpp.
|
inline |
Function to make available the matrix size in vectorization in order to optimize the gemm performance.
Definition at line 9196 of file CConfig.hpp.
|
inline |
Check if the gradient smoothing is active.
Definition at line 9837 of file CConfig.hpp.
|
inline |
Gets the factor epsilon in front of the Laplace term.
Definition at line 9843 of file CConfig.hpp.
|
inline |
Gets the factor zeta in front of the identity term.
Definition at line 9849 of file CConfig.hpp.
|
inline |
Get information about there is a smoothing of the grid coordinates.
TRUE if there is smoothing of the grid coordinates; otherwise FALSE. Definition at line 6325 of file CConfig.hpp.
|
inline |
Check if we assemble the operator on the surface.
Definition at line 9861 of file CConfig.hpp.
|
inline |
Check if we split in the dimensions.
Definition at line 9855 of file CConfig.hpp.
|
inline |
The modus of operation for the Sobolev solver.
Definition at line 9873 of file CConfig.hpp.
| bool CConfig::GetSolid_Wall | ( | unsigned short | iMarker | ) | const |
Determines whether a marker with index iMarker is a solid boundary.
| iMarker |
Definition at line 8076 of file CConfig.cpp.
|
inline |
Get the name of the file with the solution of the adjoint flow problem with drag objective function.
Definition at line 5605 of file CConfig.hpp.
|
inline |
Get the name of the file with the solution of the flow problem.
Definition at line 5597 of file CConfig.hpp.
|
inline |
Get species net reaction rates applied during spark ignition.
Definition at line 2195 of file CConfig.hpp.
|
inline |
Verify if there is mixing plane interface specified from config file.
Definition at line 5239 of file CConfig.hpp.
|
inline |
Check if the special output is written.
Definition at line 9571 of file CConfig.hpp.
|
inline |
Get the flag for activating species transport clipping.
Definition at line 2142 of file CConfig.hpp.
|
inline |
Get the maximum bound for scalar transport clipping.
Definition at line 2148 of file CConfig.hpp.
|
inline |
Get the minimum bound for scalar transport clipping.
Definition at line 2154 of file CConfig.hpp.
|
inline |
Get initial species value/concentration in the range [0,1].
Definition at line 2160 of file CConfig.hpp.
|
inline |
Get the flag for using strong BC's for in- and outlets in the species solver.
Definition at line 2166 of file CConfig.hpp.
|
inline |
Get the value of specific heat at constant pressure.
Definition at line 1700 of file CConfig.hpp.
|
inline |
Get the non-dimensional value of specific heat at constant pressure.
Definition at line 1706 of file CConfig.hpp.
|
inline |
Get parsed SST option data structure.
Definition at line 9909 of file CConfig.hpp.
|
inline |
Get the number of iterations that are not considered in the convergence criteria.
Definition at line 5810 of file CConfig.hpp.
|
inline |
Get the Starting Iteration for the windowing approach in Sensitivity Analysis for period-averaged outputs, which oscillate.
Definition at line 5642 of file CConfig.hpp.
|
inline |
Get the value of the limits for the sections.
Definition at line 1658 of file CConfig.hpp.
|
inline |
Identifies if we want to restart from a steady or an unsteady solution.
TRUE if we restart from steady state solution, FALSE otherwise. Definition at line 8947 of file CConfig.hpp.
|
inline |
Get the value of the artificial periodic outlet heat.
Definition at line 6244 of file CConfig.hpp.
|
inline |
Get the value of the pressure delta from which body force vector is computed.
Definition at line 6250 of file CConfig.hpp.
|
inline |
Get the value of the massflow from which body force vector is computed.
Definition at line 6261 of file CConfig.hpp.
|
inline |
Get information about the streamwise periodicity Energy equation handling.
Definition at line 6238 of file CConfig.hpp.
|
inline |
Get the maximum allowed VM stress and KS exponent for the stress penalty objective function.
Definition at line 9079 of file CConfig.hpp.
|
inline |
Return true if a structural solver is in use.
Definition at line 3853 of file CConfig.hpp.
|
inline |
Divide the rectbles and hexahedron.
TRUE if the elements must be divided; otherwise FALSE. Definition at line 5864 of file CConfig.hpp.
|
inline |
Get the cycle of a subsonic engine.
Definition at line 1599 of file CConfig.hpp.
|
inline |
Get the values of subsonic engine.
Definition at line 1593 of file CConfig.hpp.
|
inline |
Indicates whether supercatalytic wall is used.
Definition at line 5560 of file CConfig.hpp.
|
inline |
Provides the gas mass fractions at the wall for supercat wall.
Definition at line 5479 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8146 of file CConfig.hpp.
|
inline |
Get the density at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8181 of file CConfig.hpp.
|
inline |
Get the enthalpy at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8188 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8265 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8272 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8279 of file CConfig.hpp.
|
inline |
Get the mach number at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8160 of file CConfig.hpp.
|
inline |
Get the massflow at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8153 of file CConfig.hpp.
|
inline |
Get the momentum distortion at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
Definition at line 8223 of file CConfig.hpp.
| bool CConfig::GetSurface_Movement | ( | unsigned short | kind_movement | ) | const |
Get information about deforming markers.
| [in] | kind_movement | - Kind of surface movement. |
TRUE at least one surface of kind_movement moving; otherwise FALSE. Definition at line 8922 of file CConfig.cpp.
|
inline |
Get the normal velocity at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8195 of file CConfig.hpp.
|
inline |
Get the pressure at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8174 of file CConfig.hpp.
|
inline |
Get the pressure drop between two surfaces.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8244 of file CConfig.hpp.
|
inline |
Get the secondary flow strength at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
Definition at line 8209 of file CConfig.hpp.
|
inline |
Get the relative secondary flow strength at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
Definition at line 8216 of file CConfig.hpp.
|
inline |
Get avg species_0 at a boundary.
| [in] | val_index | - Index corresponding to the boundary. |
Definition at line 8251 of file CConfig.hpp.
|
inline |
Get the species variance at a boundary.
| [in] | val_index | - Index corresponding to the boundary. |
Definition at line 8258 of file CConfig.hpp.
|
inline |
Get the temperature at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8167 of file CConfig.hpp.
|
inline |
Get the total pressure at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8237 of file CConfig.hpp.
|
inline |
Get the total temperature at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8230 of file CConfig.hpp.
|
inline |
Get the streamwise flow uniformity at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
Definition at line 8202 of file CConfig.hpp.
|
inline |
Get the name of the file with the surface information for the adjoint problem.
Definition at line 5752 of file CConfig.hpp.
|
inline |
Get the name of the file with the surface information for the flow problem.
Definition at line 5746 of file CConfig.hpp.
|
inline |
Get the name of the file with the surface sensitivity (discrete adjoint).
Definition at line 5758 of file CConfig.hpp.
|
inline |
Governing equations of the flow (it can be different from the run time equation).
| [in] | val_zone | - Zone where the soler is applied. |
Definition at line 3919 of file CConfig.hpp.
|
inline |
Get the format of the output solution.
Definition at line 5617 of file CConfig.hpp.
|
inline |
Get the FFD Tag of a particular FFD box.
| [in] | val_ffd | - Number of the FFD box that we want to read. |
Definition at line 2960 of file CConfig.hpp.
|
inline |
Get the value specified for the target CL.
Definition at line 8734 of file CConfig.hpp.
|
inline |
Get the value of the critical temperature.
Definition at line 4026 of file CConfig.hpp.
|
inline |
Get the value of the freestream temperature.
Definition at line 1736 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream temperature.
Definition at line 1941 of file CConfig.hpp.
|
inline |
Get the value of the reference temperature for non-dimensionalization.
Definition at line 1844 of file CConfig.hpp.
|
inline |
Get the value of the freestream vibrational-electronic temperature.
Definition at line 1741 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized vibrational-electronic freestream temperature.
Definition at line 1947 of file CConfig.hpp.
|
inline |
Get the value of the reference temperature for non-dimensionalization.
Definition at line 1850 of file CConfig.hpp.
|
inline |
Get the value of the thermal conductivity.
Definition at line 4080 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensional thermal conductivity.
Definition at line 4088 of file CConfig.hpp.
|
inline |
Get the value of the reference thermal conductivity for non-dimensionalization.
Definition at line 1892 of file CConfig.hpp.
|
inline |
Get the thermal expansion coefficient.
Definition at line 2082 of file CConfig.hpp.
|
inline |
Get the non-dim. thermal expansion coefficient.
Definition at line 2088 of file CConfig.hpp.
|
inline |
Get the value of the thermal diffusivity for solids.
Definition at line 1819 of file CConfig.hpp.
|
inline |
Function to make available the multiplication factor theta of the symmetrizing terms in the DG discretization of the viscous terms.
Definition at line 9189 of file CConfig.hpp.
|
inline |
Check if the multizone problem is solved for time domain.
Definition at line 9443 of file CConfig.hpp.
|
inline |
Provides information about the time integration, and change the write in the output files information about the iteration.
Definition at line 5461 of file CConfig.hpp.
|
inline |
Get the value of the reference time for non-dimensionalization.
Definition at line 1868 of file CConfig.hpp.
|
inline |
Get the time step for multizone problems.
Definition at line 9479 of file CConfig.hpp.
|
inline |
Get the location of the time DOFs for ADER-DG on the interval [-1..1].
Definition at line 3047 of file CConfig.hpp.
|
inline |
Get the location of the time integration points for ADER-DG on the interval [-1..1].
Definition at line 3059 of file CConfig.hpp.
|
inline |
Get the current time iteration number.
| [in] | val_iter | - Current time iterationnumber. |
Definition at line 3269 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 1990 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 1978 of file CConfig.hpp.
|
inline |
Get name of output file for topology optimization derivatives.
Definition at line 9388 of file CConfig.hpp.
|
inline |
Get the i'th kernel to use, its parameter, and the radius.
Definition at line 9408 of file CConfig.hpp.
|
inline |
Number of kernels to use in filtering the design density field.
Definition at line 9403 of file CConfig.hpp.
|
inline |
Get the type and parameter for the projection function used in topology optimization.
Definition at line 9423 of file CConfig.hpp.
|
inline |
Get topology optimization.
Definition at line 9383 of file CConfig.hpp.
|
inline |
Get the maximum "logical radius" (degree of neighborhood) to consider in the neighbor search.
Definition at line 9418 of file CConfig.hpp.
|
inline |
If we are performing an unsteady simulation, this is the value of max physical time for which we run the simulation.
Definition at line 5851 of file CConfig.hpp.
|
inline |
If we are prforming an unsteady simulation, there is only one value of the time step for the complete simulation.
Definition at line 5831 of file CConfig.hpp.
|
inline |
Get the penalty weight value for the objective function.
Definition at line 9074 of file CConfig.hpp.
| su2double CConfig::GetTotalPressureIn_BC | ( | ) | const |
Get the inlet total pressure imposed as BC for internal flow.
Definition at line 9197 of file CConfig.cpp.
| su2double CConfig::GetTotalTemperatureIn_BC | ( | ) | const |
Get the inlet total temperature imposed as BC for internal flow.
Definition at line 9216 of file CConfig.cpp.
|
inline |
Get the translational velocity of the mesh.
| [in] | iDim | - spatial component |
Definition at line 5997 of file CConfig.hpp.
|
inline |
Get the value of the turbulent to laminar viscosity ratio.
Definition at line 2062 of file CConfig.hpp.
|
inline |
Get whether fixed values for turbulence quantities are applied.
TRUE if fixed values are applied; otherwise FALSE. Definition at line 8645 of file CConfig.hpp.
|
inline |
Get shift of the upstream half-plane where fixed values for turbulence quantities are applied.
This half-plane is given by the condition that the dot product between the coordinate vector and the normalized far-field velocity vector is less than what this function returns.
Definition at line 8653 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream turbulence intensity.
Definition at line 2014 of file CConfig.hpp.
|
inline |
Get the starting direct iteration number for the unsteady adjoint (reverse time integration).
Definition at line 3221 of file CConfig.hpp.
|
inline |
Get the Courant Friedrich Levi number for unsteady simulations.
Definition at line 2910 of file CConfig.hpp.
| string CConfig::GetUnsteady_FileName | ( | string | val_filename, |
| int | val_iter, | ||
| const string & | ext | ||
| ) | const |
Augment the input filename with the iteration number for an unsteady file.
| [in] | val_filename | - String value of the base filename. |
| [in] | val_iter | - Unsteady iteration number or time instance. |
| [in] | ext | - the filename extension. |
Definition at line 8365 of file CConfig.cpp.
|
inline |
Get information about whether to update the AoA for fixed lift mode.
TRUE if we should update the AoA for fixed lift mode; otherwise FALSE. Definition at line 8788 of file CConfig.hpp.
|
inline |
Get the maximum number of iterations between AoA updates for fixed C_L mode.
Definition at line 8794 of file CConfig.hpp.
|
inline |
Get the value of iterations to re-evaluate the angle of attack.
Definition at line 8764 of file CConfig.hpp.
|
inline |
Get information about whether to update the AoA for fixed lift mode.
TRUE if we should update the AoA for fixed lift mode; otherwise FALSE. Definition at line 8782 of file CConfig.hpp.
|
inline |
Get the amount of eigenvalue perturbation to be done.
Definition at line 9272 of file CConfig.hpp.
|
inline |
Get information about eigenspace perturbation.
TRUE means eigenspace perterturbation will be used Definition at line 9290 of file CConfig.hpp.
|
inline |
Get the underelaxation factor.
Definition at line 9284 of file CConfig.hpp.
|
inline |
Get whether to "Use Accurate Jacobians" for AUSM+up(2) and SLAU(2).
Definition at line 4632 of file CConfig.hpp.
|
inline |
Function to make available whether or not the lumped mass matrix must be used for steady computations.
Definition at line 9209 of file CConfig.hpp.
|
inline |
Get the name of the user scalar.
Definition at line 2240 of file CConfig.hpp.
|
inline |
Get the name of the user scalar source term.
Definition at line 2248 of file CConfig.hpp.
|
inline |
Get whether to use vectorized numerics (if available).
Definition at line 4350 of file CConfig.hpp.
|
inline |
Selection of variable density option for incompressible flows.
Definition at line 3997 of file CConfig.hpp.
|
inline |
Get the vector of the dimensionalized freestream velocity.
Definition at line 1934 of file CConfig.hpp.
|
inline |
Definition at line 1935 of file CConfig.hpp.
|
inline |
Get the vector of the non-dimensionalized freestream velocity.
Definition at line 1959 of file CConfig.hpp.
|
inline |
Definition at line 1960 of file CConfig.hpp.
|
inline |
Get the value of the reference velocity for non-dimensionalization.
Definition at line 1862 of file CConfig.hpp.
|
inline |
Get the value of limiter coefficient.
Definition at line 2490 of file CConfig.hpp.
|
inline |
Get the verification solution.
Definition at line 9378 of file CConfig.hpp.
|
inline |
Get the value of the freestream viscosity.
Definition at line 1753 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized freestream viscosity.
Definition at line 1972 of file CConfig.hpp.
|
inline |
Get the value of the reference viscosity for non-dimensionalization.
Definition at line 1874 of file CConfig.hpp.
|
inline |
Determines if problem is viscous.
Definition at line 6529 of file CConfig.hpp.
| bool CConfig::GetViscous_Wall | ( | unsigned short | iMarker | ) | const |
Determines whether a marker with index iMarker is a viscous no-slip boundary.
| iMarker |
Definition at line 8056 of file CConfig.cpp.
|
inline |
Get the node number of the CV to visualize.
Definition at line 8710 of file CConfig.hpp.
|
inline |
Get the name of the file with the volume sensitivity (discrete adjoint).
Definition at line 5764 of file CConfig.hpp.
|
inline |
Get the name of the file with the flow variables.
Definition at line 5660 of file CConfig.hpp.
|
inline |
Get the history output field iField.
Definition at line 9625 of file CConfig.hpp.
|
inline |
GetVolumeOutputFiles.
Definition at line 9721 of file CConfig.hpp.
|
inline |
GetVolumeOutputFrequency.
| [in] | iFile | index of file number for which the writing frequency needs to be returned. |
Definition at line 9732 of file CConfig.hpp.
| bool CConfig::GetVolumetric_Movement | ( | void | ) | const |
Get information about the volumetric movement.
TRUE if there is a volumetric movement is required; otherwise FALSE. Definition at line 8904 of file CConfig.cpp.
|
inline |
Get information about the Vorticity Confinement.
TRUE if it uses Vorticity Confinement; otherwise FALSE. Definition at line 6214 of file CConfig.hpp.
|
inline |
Indicates whether the VT source residual is limited.
Definition at line 5550 of file CConfig.hpp.
|
inline |
Get the name of the surface defined in the geometry file.
| [in] | val_marker | - Value of the marker in which we are interested. |
Definition at line 3945 of file CConfig.hpp.
| su2double CConfig::GetWall_Emissivity | ( | const string & | val_index | ) | const |
Get the wall emissivity at a boundary.
| [in] | val_index | - Index corresponding to the boundary. |
Definition at line 9746 of file CConfig.cpp.
|
inline |
Get information about whether to use wall functions.
TRUE if wall functions are on; otherwise FALSE. Definition at line 9296 of file CConfig.hpp.
| su2double CConfig::GetWall_HeatFlux | ( | const string & | val_index | ) | const |
Get the wall heat flux on a constant heat flux boundary.
| [in] | val_index | - Index corresponding to the constant heat flux boundary. |
Definition at line 9346 of file CConfig.cpp.
| su2double CConfig::GetWall_HeatTransfer_Coefficient | ( | const string & | val_index | ) | const |
Get the heat transfer coefficient on a heat transfer boundary.
| [in] | val_index | - Index corresponding to the heat transfer boundary. |
Definition at line 9355 of file CConfig.cpp.
| su2double CConfig::GetWall_HeatTransfer_Temperature | ( | const string & | val_index | ) | const |
Get the temperature at inifinty on a heat transfer boundary.
| [in] | val_index | - Index corresponding to the heat transfer boundary. |
Definition at line 9364 of file CConfig.cpp.
| const su2double * CConfig::GetWallFunction_DoubleInfo | ( | const string & | val_marker | ) | const |
Get the additional double info for the wall function treatment for the given boundary marker.
| [in] | val_marker | - String of the viscous wall marker. |
Definition at line 9411 of file CConfig.cpp.
| const unsigned short * CConfig::GetWallFunction_IntInfo | ( | const string & | val_marker | ) | const |
Get the additional integer info for the wall function treatment for the given boundary marker.
| [in] | val_marker | - String of the viscous wall marker. |
Definition at line 9398 of file CConfig.cpp.
| WALL_FUNCTIONS CConfig::GetWallFunction_Treatment | ( | const string & | val_marker | ) | const |
Get the wall function treatment for the given boundary marker.
| [in] | val_marker | - String of the viscous wall marker. |
Definition at line 9384 of file CConfig.cpp.
|
inline |
Get the value of the wall model constant B for turbulence wall modeling.
Definition at line 1813 of file CConfig.hpp.
|
inline |
Get the value of the von Karman constant kappa for turbulence wall modeling.
Definition at line 1789 of file CConfig.hpp.
|
inline |
Get the value of the max. number of Newton iterations for turbulence wall modeling.
Definition at line 1795 of file CConfig.hpp.
|
inline |
Get the value of the minimum Y+ value below which the wall function is deactivated.
Definition at line 1807 of file CConfig.hpp.
|
inline |
Get the value of the relaxation factor for turbulence wall modeling.
Definition at line 1801 of file CConfig.hpp.
Get the type of wall and roughness height on a wall boundary (Heatflux or Isothermal).
| [in] | val_index | - Index corresponding to the boundary. |
Definition at line 9373 of file CConfig.cpp.
|
inline |
Get the value of wall temperature.
Definition at line 1712 of file CConfig.hpp.
|
inline |
Get the heat equation.
Definition at line 9354 of file CConfig.hpp.
|
inline |
Get the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.
Definition at line 5428 of file CConfig.hpp.
|
inline |
Value of the weight of the drag coefficient in the Sonic Boom optimization.
Definition at line 6590 of file CConfig.hpp.
|
inline |
Get the weights of the time integration points for ADER-DG.
Definition at line 3065 of file CConfig.hpp.
|
inline |
Get information about the wind gust.
TRUE if there is a wind gust; otherwise FALSE. Definition at line 8602 of file CConfig.hpp.
|
inline |
Get the boolean value, whether the the Cauchy method for the time averaged windowed objective functions for unsteady flows is used or not.
Definition at line 9665 of file CConfig.hpp.
|
inline |
Get the number of iterations that are considered in the Cauchy convergence criteria for the windowed time average of the unsteady problem.
Definition at line 9645 of file CConfig.hpp.
|
inline |
Get the value of convergence criteria for the Cauchy method for the time averaged windowed objective functions for unsteady flows.
Definition at line 9652 of file CConfig.hpp.
|
inline |
Get the number of iterations that are not considered in the convergence criteria for the windowed average output function.
Definition at line 9658 of file CConfig.hpp.
|
inline |
Get functional that is going to be used to evaluate the convergence of the windowed time average of the unsteady problem.
| [in] | iField | - Index of the field |
Definition at line 9639 of file CConfig.hpp.
|
inline |
Get information about the computational graph (e.g. memory usage) when using AD in reverse mode.
TRUE means that the tape statistics will be written after each recording. Definition at line 3311 of file CConfig.hpp.
|
inline |
Check if the forces breakdown file is written.
Definition at line 9577 of file CConfig.hpp.
|
inline |
Get information about writing the mesh quality metrics to the visualization files.
TRUE means that the mesh quality metrics will be written to the visualization files. Definition at line 3317 of file CConfig.hpp.
|
inline |
Write coarse grids to the visualization files.
Definition at line 3322 of file CConfig.hpp.
|
inline |
Get information about writing the performance summary at the end of a calculation.
TRUE means that the performance summary will be written at the end of a calculation. Definition at line 3305 of file CConfig.hpp.
|
inline |
Get information about writing projected sensitivities on surfaces to an ASCII file with rows as x, y, z, dJ/dx, dJ/dy, dJ/dz for each vertex.
TRUE means that projected sensitivities on surfaces in an ASCII file with rows as x, y, z, dJ/dx, dJ/dy, dJ/dz for each vertex will be written. Definition at line 3328 of file CConfig.hpp.
|
inline |
Flag for whether restart solution files are overwritten.
Definition at line 5497 of file CConfig.hpp.
|
inline |
Flag for whether visualization files are overwritten.
Definition at line 5503 of file CConfig.hpp.
|
inline |
Flag for whether visualization files are overwritten.
Definition at line 5509 of file CConfig.hpp.
|
inline |
Check if the convergence history of each individual zone is written to screen.
Definition at line 9559 of file CConfig.hpp.
|
inline |
Check if the convergence history of each individual zone is written to file.
Definition at line 9565 of file CConfig.hpp.
| void CConfig::Init | ( | ) |
Initialize common fields of the config structure.
Definition at line 264 of file CConfig.cpp.
|
inline |
Get information about the Low Mach Correction.
TRUE if we are using low Mach correction; otherwise FALSE. Definition at line 6196 of file CConfig.hpp.
|
inline |
Get information about the Low Mach Preconditioning.
TRUE if we are using low Mach preconditioner; otherwise FALSE. Definition at line 6190 of file CConfig.hpp.
|
inline |
Check if an option is present in the config file.
| [in] | - | Name of the option |
Definition at line 9757 of file CConfig.hpp.
|
inline |
Set the values for the electric field modulus.
| [in] | val_coeff | - Index of the electric field. |
| [in] | val_el_field | - Value of the electric field. |
Definition at line 9016 of file CConfig.hpp.
|
inline |
Set the start time to track a phase of the code (preprocessing, compute, output).
| [in] | Value | of the start time to track a phase of the code. |
Definition at line 9683 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8083 of file CConfig.hpp.
| void CConfig::SetActDisk_BCThrust | ( | const string & | val_marker, |
| su2double | val_actdisk_bcthrust | ||
| ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8779 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8055 of file CConfig.hpp.
| void CConfig::SetActDisk_BCThrust_Old | ( | const string & | val_marker, |
| su2double | val_actdisk_bcthrust_old | ||
| ) |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8787 of file CConfig.cpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8069 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7789 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8006 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7817 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8076 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7810 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7803 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8041 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7796 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8027 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8034 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8013 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8020 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8104 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7635 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8111 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7775 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8097 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8090 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7572 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7782 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7579 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8356 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8349 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7649 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8363 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8335 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7600 of file CConfig.hpp.
|
inline |
Set the thrust at the outlet (actuator disk) boundary.
| [in] | val_marker | - Marker corresponding to the outlet (actuator disk) boundary. |
| [in] | val_actdisk_thrust_bem | - Value of the actuator disk thrust. |
Definition at line 8370 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Marker corresponding to the outlet boundary. |
| [in] | val_actdisk_torque_bem | - Value of the actuator disk torque. |
Definition at line 8379 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 8342 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7607 of file CConfig.hpp.
|
inline |
Value of Aeroelastic solution coordinate at time n from time n+1.
Definition at line 8522 of file CConfig.hpp.
|
inline |
Value of Aeroelastic solution coordinate at time n-1 from time n.
Definition at line 8527 of file CConfig.hpp.
|
inline |
Value of Aeroelastic solution coordinate at time n+1.
Definition at line 8517 of file CConfig.hpp.
|
inline |
Value of pitching coordinate.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val | - value of pitching coordinate. |
Definition at line 8590 of file CConfig.hpp.
|
inline |
Value of plunging coordinate.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val | - value of plunging coordinate. |
Definition at line 8583 of file CConfig.hpp.
|
inline |
Set the angle of attack.
| [in] | val_AoA | - Value of the angle of attack. |
Definition at line 2816 of file CConfig.hpp.
|
inline |
Set the off set angle of attack.
| [in] | val_AoA | - Value of the angle of attack. |
Definition at line 2822 of file CConfig.hpp.
|
inline |
Set the angle of attack.
| [in] | val_AoA | - Value of the angle of attack. |
Definition at line 2834 of file CConfig.hpp.
|
inline |
Set the angle of attack.
| [in] | val_AoA | - Value of the angle of attack. |
Definition at line 2840 of file CConfig.hpp.
|
inline |
Set the off set sideslip angle.
| [in] | val_AoA | - Value of the off set sideslip angle. |
Definition at line 2828 of file CConfig.hpp.
|
inline |
Get the Courant Friedrich Levi number for each grid.
| [in] | val_mesh | - Index of the mesh were the CFL is applied. |
Definition at line 2904 of file CConfig.hpp.
|
inline |
Set the reference conductivity for nondimensionalization.
| [in] | val_conductivity_ref | - Value of the reference conductivity. |
Definition at line 2624 of file CConfig.hpp.
| void CConfig::SetConfig_Parsing | ( | char | case_filename[MAX_STRING_SIZE] | ) |
Set the config file parsing.
Definition at line 2977 of file CConfig.cpp.
| void CConfig::SetConfig_Parsing | ( | istream & | config_buffer | ) |
Set the config file parsing.
Definition at line 2995 of file CConfig.cpp.
|
inline |
Set the temperature polynomial coefficient for specific heat Cp.
| [in] | val_coeff | - Temperature polynomial coefficient for specific heat Cp. |
| [in] | val_index | - Index of the array with all polynomial coefficients. |
Definition at line 4225 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6614 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6656 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6626 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6638 of file CConfig.hpp.
|
inline |
Value of the weight of the CD, CL, CM optimization.
Definition at line 6650 of file CConfig.hpp.
|
inline |
Set the value of the unsteadty time step using the CFL number.
| [in] | val_delta_unsttimend | - Value of the unsteady time step using CFL number. |
Definition at line 5844 of file CConfig.hpp.
|
inline |
Set the freestream density.
| [in] | val_density_freestream | - Value of the freestream density. |
Definition at line 2660 of file CConfig.hpp.
|
inline |
Set the nondimensionalized freestream density.
| [in] | val_density_freestreamnd | - Value of the nondimensionalized freestream density. |
Definition at line 2654 of file CConfig.hpp.
|
inline |
Set the reference pressure for nondimensionalization.
| [in] | val_density_ref | - Value of the reference pressure. |
Definition at line 2558 of file CConfig.hpp.
|
inline |
Set the value of the non-dimensional constant mass diffusivity.
Definition at line 4244 of file CConfig.hpp.
| void CConfig::SetdNetThrust_dBCThrust | ( | su2double | val_dnetthrust_dbcthrust | ) |
Value of the damping factor for the Thrust BC (actuator disk).
|
inline |
Set the value of the domain volume computed on the finest grid.
| [in] | val_volume | - Value of the domain volume computed on the finest grid. |
Definition at line 2454 of file CConfig.hpp.
|
inline |
Set the value of the design variable step, we use this value in design problems.
| [in] | val_dv | - Number of the design variable that we want to read. |
| [in] | val_ind | - value of initial deformation. |
| [in] | val | - Value of the design variable. |
Definition at line 5899 of file CConfig.hpp.
|
inline |
Set the freestream energy.
| [in] | val_energy_freestream | - Value of the freestream energy. |
Definition at line 2770 of file CConfig.hpp.
|
inline |
Set the non-dimensional freestream energy.
| [in] | val_energy_freestreamnd | - Value of the non-dimensional freestream energy. |
Definition at line 2764 of file CConfig.hpp.
|
inline |
Set the reference energy for nondimensionalization.
| [in] | val_energy_ref | - Value of the reference energy. |
Definition at line 2582 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_area | - Exhaust power. |
Definition at line 7522 of file CConfig.hpp.
|
inline |
Set the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_force | - Exhaust power. |
Definition at line 7494 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_grossthrust | - Exhaust power. |
Definition at line 7515 of file CConfig.hpp.
|
inline |
Set the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_mach | - Exhaust power. |
Definition at line 7487 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_netthrust | - Exhaust power. |
Definition at line 7508 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_marker | - Index corresponding to a particular engine boundary. |
| [in] | val_engine_power | - Exhaust power. |
Definition at line 7501 of file CConfig.hpp.
|
inline |
Set boolean for using Persson's shock capturing method in Euler flow DG-FEM.
| [in] | val_EulerPersson | - Boolean for using Persson's shock capturing method in Euler flow DG-FEM |
Definition at line 9103 of file CConfig.hpp.
|
inline |
Set the force balance at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_force | - Exhaust force balance. |
Definition at line 7473 of file CConfig.hpp.
|
inline |
Set the gross thrust at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_grossthrust | - Exhaust gross thrust temperature. |
Definition at line 7466 of file CConfig.hpp.
|
inline |
Set the back pressure (static) at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_temp | - Exhaust static temperature. |
Definition at line 7445 of file CConfig.hpp.
|
inline |
Set the power at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_power | - Exhaust power. |
Definition at line 7480 of file CConfig.hpp.
|
inline |
Set the back pressure (static) at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_pressure | - Exhaust static pressure. |
Definition at line 7431 of file CConfig.hpp.
|
inline |
Set the temperature (static) at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_temp | - Exhaust static temperature. |
Definition at line 7438 of file CConfig.hpp.
|
inline |
Set the back pressure (total) at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_totalpressure | - Exhaust total pressure. |
Definition at line 7452 of file CConfig.hpp.
|
inline |
Set the total temperature at an engine exhaust boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
| [in] | val_exhaust_totaltemp | - Exhaust total temperature. |
Definition at line 7459 of file CConfig.hpp.
|
inline |
Set the current external iteration number.
| [in] | val_iter | - Current external iteration number. |
Definition at line 3245 of file CConfig.hpp.
|
inline |
Set the finest mesh in a multigrid strategy.
| [in] | val_finestmesh | - Index of the finest grid. |
Definition at line 2462 of file CConfig.hpp.
|
inline |
Set whether at the end of finite differencing (Fixed CL mode)
Definition at line 8805 of file CConfig.hpp.
|
inline |
Set the reference Force for nondimensionalization.
| [in] | val_force_ref | - Value of the reference Force. |
Definition at line 2594 of file CConfig.hpp.
| void CConfig::SetFreeStreamTurboNormal | ( | const su2double * | turboNormal | ) |
Set freestream turbonormal for initializing solution.
Definition at line 10188 of file CConfig.cpp.
|
inline |
Set the Froude number for free surface problems.
| [in] | val_froude | - Value of the Froude number. |
Definition at line 2522 of file CConfig.hpp.
|
inline |
Set the gas-constant.
| [in] | val_gas_constant | - Value of the gas-constant. |
Definition at line 2606 of file CConfig.hpp.
|
inline |
Set the reference gas-constant for nondimensionalization.
| [in] | val_gas_constant_ref | - Value of the reference gas-constant. |
Definition at line 2600 of file CConfig.hpp.
|
inline |
Set the non-dimensional gas-constant.
| [in] | val_gas_constantnd | - Value of the non-dimensional gas-constant. |
Definition at line 2708 of file CConfig.hpp.
| void CConfig::SetGiles_Var1 | ( | su2double | newVar1, |
| const string & | val_marker | ||
| ) |
Set the var 1 for Giles BC.
| [in] | val_marker | - Index corresponding to the Giles BC. |
Definition at line 9125 of file CConfig.cpp.
| void CConfig::SetGlobalParam | ( | MAIN_SOLVER | val_solver, |
| unsigned short | val_system | ||
| ) |
Set the global parameters of each simulation for each runtime system.
| [in] | val_solver | - Solver of the simulation. |
| [in] | val_system | - Runtime system that we are solving. |
Definition at line 8553 of file CConfig.cpp.
| void CConfig::SetHeader | ( | SU2_COMPONENT | val_software | ) | const |
Print the header to screen.
| val_software | - Kind of software component |
Definition at line 3263 of file CConfig.cpp.
|
inline |
Set the heat flux reference value.
Definition at line 2612 of file CConfig.hpp.
Set the position of the center of the volumetric heat source.
| [in] | x_cent | = X position of the center of the volumetric heat source. |
| [in] | y_cent | = Y position of the center of the volumetric heat source. |
| [in] | z_cent | = Z position of the center of the volumetric heat source. |
Definition at line 6299 of file CConfig.hpp.
|
inline |
Set the rotation angle of the volumetric heat source in axis Z.
| [in] | val_rot | - Rotation (Z) of the volumetric heat source |
Definition at line 6285 of file CConfig.hpp.
|
inline |
SetHistory_Wrt_Freq_Inner.
| [in] | iter | index for Time (0), Outer (1), or Inner (2) iterations |
| [in] | nIter | Number of iterations |
Definition at line 9702 of file CConfig.hpp.
|
inline |
Set the current instance.
| [in] | iInst | - current instance identifier. |
Definition at line 8959 of file CConfig.hpp.
| void CConfig::SetIncInlet_BC | ( | su2double | val_in | ) |
Set the inlet velocity or pressure imposed as BC for incompressible flow.
| [in] | val_in | - New value of the inlet velocity or pressure. |
Definition at line 9289 of file CConfig.cpp.
| void CConfig::SetIncPressureOut_BC | ( | su2double | val_pressure | ) |
Set the outlet pressure imposed as BC for incompressible flow.
| [in] | val_pressure | - New value of the outlet pressure. |
Definition at line 9327 of file CConfig.cpp.
| void CConfig::SetIncTemperature_BC | ( | su2double | val_temperature | ) |
Set the inlet temperature imposed as BC for incompressible flow.
| [in] | val_temperature | - New value of the inlet temperature. |
Definition at line 9309 of file CConfig.cpp.
|
inline |
Set the force balance at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_force | - Fan face force. |
Definition at line 7417 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7361 of file CConfig.hpp.
|
inline |
Set the massflow at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_massflow | - Massflow. |
Definition at line 7375 of file CConfig.hpp.
|
inline |
Set the power at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_force | - Power. |
Definition at line 7424 of file CConfig.hpp.
|
inline |
Set the fan face static pressure at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_pressure | - Fan face static pressure. |
Definition at line 7368 of file CConfig.hpp.
|
inline |
Set the ram drag temperature at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_ramdrag | - Ram drag value. |
Definition at line 7410 of file CConfig.hpp.
|
inline |
Set the reverse flow at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_reversemassflow | - reverse flow. |
Definition at line 7382 of file CConfig.hpp.
|
inline |
Set the fan face static temperature at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_pressure | - Fan face static temperature. |
Definition at line 7396 of file CConfig.hpp.
|
inline |
Set the fan face total pressure at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_totalpressure | - Fan face total pressure. |
Definition at line 7389 of file CConfig.hpp.
|
inline |
Set the fan face total temperature at an engine inflow boundary.
| [in] | val_index | - Index corresponding to the engine inflow boundary. |
| [in] | val_fanface_totaltemperature | - Fan face total temperature. |
Definition at line 7403 of file CConfig.hpp.
|
inline |
Get the value of the non-dimensionalized actuator disk turbulence intensity.
Definition at line 2056 of file CConfig.hpp.
| void CConfig::SetInletPtotal | ( | su2double | val_pressure, |
| const string & | val_marker | ||
| ) |
Set the total pressure at an inlet boundary.
| [in] | val_pressure | - Pressure value at the inlet boundary. |
| [in] | val_index | - Index corresponding to the inlet boundary. |
Definition at line 9023 of file CConfig.cpp.
|
inline |
Set the current FSI iteration number.
| [in] | val_iter | - Current FSI iteration number. |
Definition at line 3257 of file CConfig.hpp.
|
inline |
Set the kind of mixing process for averaging quantities at the boundaries.
Definition at line 5138 of file CConfig.hpp.
| void CConfig::SetKind_ConvNumScheme | ( | unsigned short | val_kind_convnumscheme, |
| CENTERED | val_kind_centered, | ||
| UPWIND | val_kind_upwind, | ||
| LIMITER | val_kind_slopelimit, | ||
| bool | val_muscl, | ||
| unsigned short | val_kind_fem | ||
| ) |
Set the parameters of the convective numerical scheme.
| [in] | val_kind_convnumscheme | - Center or upwind scheme. |
| [in] | val_kind_centered | - If centered scheme, kind of centered scheme (JST, etc.). |
| [in] | val_kind_upwind | - If upwind scheme, kind of upwind scheme (Roe, etc.). |
| [in] | val_kind_slopelimit | - If upwind scheme, kind of slope limit. |
| [in] | val_muscl | - Define if we apply a MUSCL scheme or not. |
| [in] | val_kind_fem | - If FEM, what kind of FEM discretization. |
Definition at line 8540 of file CConfig.cpp.
|
inline |
Set the type of dynamic mesh motion.
| [in] | motion_Type | - Specify motion type. |
Definition at line 5946 of file CConfig.hpp.
|
inline |
Set the kind of mixing process for averaging quantities at the boundaries.
Definition at line 5144 of file CConfig.hpp.
|
inline |
Set the kind of SU2 software component.
Definition at line 4488 of file CConfig.hpp.
|
inline |
Set the kind of time integration scheme.
| [in] | val_kind_timeintscheme | - Kind of time integration scheme. |
Definition at line 2470 of file CConfig.hpp.
| void CConfig::SetKindWall | ( | string | val_marker, |
| unsigned short | val_kindwall | ||
| ) |
Set the kind of wall - rough or smooth.
|
inline |
Set the temperature polynomial coefficient for thermal conductivity.
| [in] | val_coeff | - Non-dimensional temperature polynomial coefficient for thermal conductivity. |
| [in] | val_index | - Index of the array with all polynomial coefficients. |
Definition at line 4239 of file CConfig.hpp.
|
inline |
Set the reference length for nondimensionalization.
| [in] | val_length_ref | - Value of the reference length. |
Definition at line 2540 of file CConfig.hpp.
|
inline |
Set the Mach number.
| [in] | val_mach | - Value of the Mach number. |
Definition at line 2528 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be plot val_plotting (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_plotting | - 0 or 1 depending if the the marker is going to be plot. |
Definition at line 3490 of file CConfig.hpp.
|
inline |
Set if a marker val_marker allows deformation at the boundary.
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_interface | - 0 or 1 depending if the the marker is or not a DEFORM_MESH marker. |
Definition at line 3556 of file CConfig.hpp.
|
inline |
Set if a marker val_marker allows deformation at the boundary.
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_interface | - 0 or 1 depending if the the marker is or not a DEFORM_MESH_SYM_PLANE marker. |
Definition at line 3563 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be designed val_designing (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_monitoring | - 0 or 1 depending if the the marker is going to be designed. |
Definition at line 3474 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be affected by design variables val_moving (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_DV | - 0 or 1 depending if the the marker is affected by design variables. |
Definition at line 3534 of file CConfig.hpp.
|
inline |
Set if a in marker val_marker the flow load will be computed/employed.
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_interface | - 0 or 1 depending if the the marker is or not a Fluid_Load marker. |
Definition at line 3570 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be monitored val_monitoring (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_monitoring | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 3465 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is part of the Giles boundary (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_giles | - 0 if not part of the Giles boundary or greater than 1 if it is part. |
Definition at line 3526 of file CConfig.hpp.
|
inline |
Set the value of the boundary val_boundary (read from the config file) for the marker val_marker.
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_boundary | - Kind of boundary read from config file. |
Definition at line 3439 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is part of the MixingPlane interface (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_turboperf | - 0 if not part of the MixingPlane interface or greater than 1 if it is part. |
Definition at line 3519 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be monitored val_monitoring (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_monitoring | - 0 or 1 depending if the the marker is going to be monitored. |
Definition at line 3456 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be moved val_moving (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_moving | - 0 or 1 depending if the the marker is going to be moved. |
Definition at line 3542 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be periodic val_perbound (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_perbound | - Index of the surface with the periodic boundary. |
Definition at line 3586 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be plot val_plotting (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_plotting | - 0 or 1 depending if the the marker is going to be plot. |
Definition at line 3482 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be customized in Python val_PyCustom (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_PyCustom | - 0 or 1 depending if the the marker is going to be customized in Python. |
Definition at line 3578 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is going to be sent or receive val_index from another domain.
| [in] | val_marker | - 0 or 1 depending if the the marker is going to be moved. |
| [in] | val_index | - Index of the surface read from geometry file. |
Definition at line 3594 of file CConfig.hpp.
|
inline |
Set if a marker how val_marker is going to be applied in gradient treatment.
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_sobolev | - 0 or 1 depending if the marker is selected. |
Definition at line 3549 of file CConfig.hpp.
|
inline |
Set the value of the index val_index (read from the geometry file) for the marker val_marker.
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_index | - Index of the surface read from geometry file. |
Definition at line 3447 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is part of the Turbomachinery (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_turboperf | - 0 if not part of Turbomachinery or greater than 1 if it is part. |
Definition at line 3505 of file CConfig.hpp.
|
inline |
Set a flag to the marker val_marker part of the Turbomachinery (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_turboperflag | - 0 if is not part of the Turbomachinery, flag INFLOW or OUTFLOW if it is part. |
Definition at line 3512 of file CConfig.hpp.
|
inline |
Set if a marker val_marker is part of the FSI interface val_plotting (read from the config file).
| [in] | val_marker | - Index of the marker in which we are interested. |
| [in] | val_plotting | - 0 or 1 depending if the the marker is part of the FSI interface. |
Definition at line 3498 of file CConfig.hpp.
|
inline |
Set the mesh motion origin.
| [in] | val | - new value of the origin |
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) |
Definition at line 5988 of file CConfig.hpp.
|
inline |
Set the rotation rate of the marker.
| [in] | iMarkerMoving | - Index of the moving marker (as specified in Marker_Moving) |
| [in] | iDim | - spatial component |
| [in] | val | - Rotational velocity |
Definition at line 6052 of file CConfig.hpp.
| void CConfig::SetMarkers | ( | SU2_COMPONENT | val_software | ) |
Config file markers processing.
Definition at line 5604 of file CConfig.cpp.
|
inline |
Set the translation rate of the marker.
| [in] | iDim | - spatial component |
| [in] | val | - translational velocity |
Definition at line 6019 of file CConfig.hpp.
|
inline |
Set the maximum velocity^2 in the domain for the incompressible preconditioner.
| [in] | Value | of the maximum velocity^2 in the domain for the incompressible preconditioner. |
Definition at line 9307 of file CConfig.hpp.
|
inline |
Set the number of multigrid levels.
| [in] | val_nMGLevels | - Index of the mesh were the CFL is applied |
Definition at line 2865 of file CConfig.hpp.
|
inline |
Set the magnitude of the free-stream velocity.
| [in] | val_modvel_freestream | - Magnitude of the free-stream velocity. |
Definition at line 2672 of file CConfig.hpp.
|
inline |
Set the non-dimensional magnitude of the free-stream velocity.
| [in] | val_modvel_freestreamnd | - Non-dimensional magnitude of the free-stream velocity. |
Definition at line 2678 of file CConfig.hpp.
|
inline |
Set Monitor Outlet Pressure value for the ramp.
Definition at line 5179 of file CConfig.hpp.
|
inline |
Set the mesh motion origin.
| [in] | val | - new value of the origin |
Definition at line 5973 of file CConfig.hpp.
| void CConfig::SetMPICommunicator | ( | SU2_MPI::Comm | Communicator | ) |
Set the MPI communicator for SU2.
| [in] | Communicator | - MPI communicator for SU2. |
Definition at line 281 of file CConfig.cpp.
|
inline |
Set the temperature polynomial coefficient for viscosity.
| [in] | val_coeff | - Non-dimensional temperature polynomial coefficient for viscosity. |
| [in] | val_index | - Index of the array with all polynomial coefficients. |
Definition at line 4232 of file CConfig.hpp.
| void CConfig::SetMultizone | ( | const CConfig * | driver_config, |
| const CConfig *const * | config_container | ||
| ) |
Set multizone properties.
Definition at line 10196 of file CConfig.cpp.
|
inline |
Set that the simulation we are running is a multizone simulation.
| [in] | MZ_problem | - boolean that determines is Multizone_Problem is true/false. |
Definition at line 9121 of file CConfig.hpp.
|
inline |
number Turbomachinery blades computed using the pitch information.
Definition at line 5263 of file CConfig.hpp.
| void CConfig::SetnDim | ( | ) |
Set the physical dimension of the problem.
|
inline |
Set the number of time levels for time accurate local time stepping.
| [in] | val_nLevels | - The number of time levels to be set. |
Definition at line 3035 of file CConfig.hpp.
|
inline |
Stores the number of marker in the simulation.
| [in] | val_nmarker | - Number of markers of the problem. |
Definition at line 3215 of file CConfig.hpp.
|
inline |
Set the current number of non-physical nodes in the solution.
| [in] | val_nonphys_points | - current number of non-physical points. |
Definition at line 8811 of file CConfig.hpp.
|
inline |
Set the current number of non-physical reconstructions for 2nd-order upwinding.
| [in] | val_nonphys_reconstr | - current number of non-physical reconstructions for 2nd-order upwinding. |
Definition at line 8823 of file CConfig.hpp.
|
inline |
set number span-wise sections to compute 3D BC and performance for turbomachinery.
Definition at line 5337 of file CConfig.hpp.
|
inline |
set number of maximum span-wise sections among all zones .
Definition at line 5316 of file CConfig.hpp.
|
inline |
set number span-wise sections to compute 3D BC and performance for turbomachinery.
Definition at line 5327 of file CConfig.hpp.
|
inline |
Set the number of time iterations.
| [in] | val_iter | - Number of time steps run |
Definition at line 9467 of file CConfig.hpp.
| void CConfig::SetnZone | ( | ) |
Set the number of zones.
Definition at line 3304 of file CConfig.cpp.
|
inline |
Set the freestream specific dissipation rate omega.
| [in] | val_omega_freestream | - Value of the freestream specific dissipation rate omega. |
Definition at line 2752 of file CConfig.hpp.
|
inline |
Set the non-dimensional freestream specific dissipation rate omega.
| [in] | val_omega_freestreamnd | - Value of the non-dimensional freestream specific dissipation rate omega. |
Definition at line 2740 of file CConfig.hpp.
|
inline |
Set the reference Omega for nondimensionalization.
| [in] | val_omega_ref | - Value of the reference omega. |
Definition at line 2588 of file CConfig.hpp.
|
inline |
Set the scale factor for the line search.
| [in] | val_scale | - scale of the deformation. |
Definition at line 8704 of file CConfig.hpp.
|
inline |
Set the current FSI iteration number.
| [in] | val_iter | - Current FSI iteration number. |
Definition at line 3251 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7859 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7845 of file CConfig.hpp.
|
inline |
Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7831 of file CConfig.hpp.
| void CConfig::SetOutlet_Pressure | ( | su2double | val_pressure, |
| const string & | val_marker | ||
| ) |
Set the back pressure (static) at an outlet boundary.
| [in] | val_pressure | - Pressure value at the outlet boundary. |
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 9083 of file CConfig.cpp.
| void CConfig::SetOutput | ( | SU2_COMPONENT | val_software, |
| unsigned short | val_izone | ||
| ) |
Config file output.
Definition at line 6168 of file CConfig.cpp.
|
inline |
Set the current physical time.
| [in] | val_t | - Current physical time. |
Definition at line 3293 of file CConfig.hpp.
| void CConfig::SetPointersNull | ( | void | ) |
Initializes pointers to null.
Definition at line 824 of file CConfig.cpp.
| void CConfig::SetPostprocessing | ( | SU2_COMPONENT | val_software, |
| unsigned short | val_izone, | ||
| unsigned short | val_nDim | ||
| ) |
Config file postprocessing.
Definition at line 3364 of file CConfig.cpp.
|
inline |
Define preferential diffusion combustion problem.
Definition at line 2207 of file CConfig.hpp.
|
inline |
Set the freestream pressure.
| [in] | val_pressure_freestream | - Value of the freestream pressure. |
Definition at line 2636 of file CConfig.hpp.
|
inline |
Set the nondimensionalized freestream pressure.
| [in] | val_pressure_freestreamnd | - Value of the nondimensionalized freestream pressure. |
Definition at line 2630 of file CConfig.hpp.
|
inline |
Set the reference pressure for nondimensionalization.
| [in] | val_pressure_ref | - Value of the reference pressure. |
Definition at line 2552 of file CConfig.hpp.
|
inline |
Set the thermodynamic pressure for low Mach problems.
Definition at line 2648 of file CConfig.hpp.
|
inline |
Set the non-dimensionalized thermodynamic pressure for low Mach problems.
Definition at line 2642 of file CConfig.hpp.
| void CConfig::SetPressureOut_BC | ( | su2double | val_press | ) |
Set the outlet pressure imposed as BC for internal flow.
| [in] | val_temp | - New value of the outlet pressure. |
Definition at line 9183 of file CConfig.cpp.
| void CConfig::SetProfilingCSV | ( | void | ) |
Write a CSV file containing the results of the profiling.
Definition at line 9804 of file CConfig.cpp.
|
inline |
In case the RefArea is equal to 0 then, it is necessary to compute a reference area, with this function we set the value of the reference area.
| [in] | val_area | - Value of the reference area for non dimensional coefficient computation. |
Definition at line 2440 of file CConfig.hpp.
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Set reference origin x-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val_origin | - New x-coordinate of the mesh motion origin. |
Definition at line 1540 of file CConfig.hpp.
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Set reference origin y-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val_origin | - New y-coordinate of the mesh motion origin. |
Definition at line 1547 of file CConfig.hpp.
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Set reference origin z-coordinate for moment computation.
| [in] | val_marker | - the marker we are monitoring. |
| [in] | val_origin | - New z-coordinate of the mesh motion origin. |
Definition at line 1554 of file CConfig.hpp.
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Set the sum of the bandwidth for writing binary restarts (to be averaged later).
| [in] | Sum | of the bandwidth for writing binary restarts. |
Definition at line 9319 of file CConfig.hpp.
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Set the freestream momentum thickness Reynolds number.
| [in] | val_ReThetaT_freestream | - Value of the freestream momentum thickness Reynolds number. |
Definition at line 2758 of file CConfig.hpp.
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Set the Reynolds number.
| [in] | val_reynolds | - Value of the Reynolds number. |
Definition at line 2534 of file CConfig.hpp.
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Get the rotation rate of the mesh.
| [in] | iDim | - spatial component |
| [in] | val | - new value of the rotation rate. |
Definition at line 6036 of file CConfig.hpp.
| void CConfig::SetRotation_Rate_Z | ( | su2double | newRotation_Rate_Z | ) |
Set the angular velocity of the mesh about the z-axis.
| [in] | newRotation_Rate_Z | - new rotation rate after computing the ramp value. |
| bool CConfig::SetRunTime_Parsing | ( | char | case_filename[MAX_STRING_SIZE] | ) |
Set the config file parsing.
Definition at line 3174 of file CConfig.cpp.
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SetScreen_Wrt_Freq_Inner.
| [in] | iter | index for Time (0), Outer (1), or Inner (2) iterations |
| [in] | nIter | Number of iterations |
Definition at line 9716 of file CConfig.hpp.
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In case the SemiSpan is equal to 0 then, it is necessary to compute the max y distance, with this function we set the value of the semi span.
| [in] | val_semispan | - Value of the semispan. |
Definition at line 2447 of file CConfig.hpp.
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Set the value of the pressure delta from which body force vector is computed. Necessary for Restart metadata.
Definition at line 6255 of file CConfig.hpp.
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Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7866 of file CConfig.hpp.
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Set the density at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_density | - Value of the density. |
Definition at line 7901 of file CConfig.hpp.
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Set the enthalpy at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_density | - Value of the density. |
Definition at line 7908 of file CConfig.hpp.
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Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7985 of file CConfig.hpp.
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Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7992 of file CConfig.hpp.
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Get the back pressure (static) at an outlet boundary.
| [in] | val_index | - Index corresponding to the outlet boundary. |
Definition at line 7999 of file CConfig.hpp.
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Set the mach number at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_massflow | - Value of the mach number. |
Definition at line 7880 of file CConfig.hpp.
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Set the massflow at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_massflow | - Value of the mass flow. |
Definition at line 7873 of file CConfig.hpp.
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Set the momentum distortion at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_momentumdistortion | - Value of the momentum distortion. |
Definition at line 7943 of file CConfig.hpp.
| void CConfig::SetSurface_Movement | ( | unsigned short | iMarker, |
| unsigned short | kind_movement | ||
| ) |
Set a surface movement marker.
| [in] | iMarker | - Moving marker. |
| [in] | kind_movement | - Kind of surface movement. |
TRUE at least one surface of kind_movement moving; otherwise FALSE. Definition at line 8082 of file CConfig.cpp.
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Set the normal velocity at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_normalvelocity | - Value of the normal velocity. |
Definition at line 7915 of file CConfig.hpp.
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Set the pressure at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_massflow | - Value of the pressure. |
Definition at line 7894 of file CConfig.hpp.
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Set the pressure drop between two surfaces.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_pressuredrop | - Value of the pressure drop. |
Definition at line 7964 of file CConfig.hpp.
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Set the secondary flow strength at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_secondarystrength | - Value of the secondary flow strength. |
Definition at line 7929 of file CConfig.hpp.
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Set the relative secondary flow strength at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_secondaryoverstream | - Value of the relative seondary flow strength. |
Definition at line 7936 of file CConfig.hpp.
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Set the average of species_0 at the surface.
| [in] | val_marker | - Index corresponding to boundary. |
| [in] | val_surface_species_0 | - Value of avg species_0. |
Definition at line 7971 of file CConfig.hpp.
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Set the species variance at the surface.
| [in] | val_marker | - Index corresponding to boundary. |
| [in] | val_surface_species_variance | - Value of the species variance. |
Definition at line 7978 of file CConfig.hpp.
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Set the temperature at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_massflow | - Value of the temperature. |
Definition at line 7887 of file CConfig.hpp.
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Set the total pressure at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_totalpressure | - Value of the total pressure. |
Definition at line 7957 of file CConfig.hpp.
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Set the total temperature at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_totaltemperature | - Value of the total temperature. |
Definition at line 7950 of file CConfig.hpp.
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Set the streamwise flow uniformity at the surface.
| [in] | val_marker | - Index corresponding to the outlet boundary. |
| [in] | val_surface_streamwiseuniformity | - Value of the streamwise flow uniformity. |
Definition at line 7922 of file CConfig.hpp.
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Set the freestream temperature.
| [in] | val_temperature_freestream | - Value of the freestream temperature. |
Definition at line 2684 of file CConfig.hpp.
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Set the non-dimensional freestream temperature.
| [in] | val_temperature_freestreamnd | - Value of the non-dimensional freestream temperature. |
Definition at line 2690 of file CConfig.hpp.
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Set the reference temperature for nondimensionalization.
| [in] | val_temperature_ref | - Value of the reference temperature. |
Definition at line 2564 of file CConfig.hpp.
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Set the freestream vibrational-electronic temperature.
| [in] | val_temperature_ve_freestream | - Value of the freestream vibrational-electronic temperature. |
Definition at line 2696 of file CConfig.hpp.
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Set the non-dimensional freestream vibrational-electronic temperature.
| [in] | val_temperature_ve_freestreamnd | - Value of the non-dimensional freestream vibrational-electronic temperature. |
Definition at line 2702 of file CConfig.hpp.
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Set the reference temperature.
| [in] | val_temperature_ve_ref | - Value of the reference temperature. |
Definition at line 2570 of file CConfig.hpp.
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Set the thermal expansion coefficient.
| [in] | val_thermal_expansion | - thermal expansion coefficient |
Definition at line 2094 of file CConfig.hpp.
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Set the non-dim. thermal expansion coefficient.
| [in] | val_thermal_expansion | - non-dim. thermal expansion coefficient |
Definition at line 2100 of file CConfig.hpp.
|
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Set the thermal diffusivity for solids.
| [in] | val_thermal_diffusivity | - Value of the thermal diffusivity. |
Definition at line 2776 of file CConfig.hpp.
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Set the reference time for nondimensionalization.
| [in] | val_time_ref | - Value of the reference time. |
Definition at line 2576 of file CConfig.hpp.
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Set the current time iteration number.
| [in] | val_iter | - Current FSI iteration number. |
Definition at line 3263 of file CConfig.hpp.
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Set the freestream turbulent kinetic energy.
| [in] | val_tke_freestream | - Value of the freestream turbulent kinetic energy. |
Definition at line 2746 of file CConfig.hpp.
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Set the non-dimensional freestream turbulent kinetic energy.
| [in] | val_tke_freestreamnd | - Value of the non-dimensional freestream turbulent kinetic energy. |
Definition at line 2734 of file CConfig.hpp.
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Set the non-dimensional total time for unsteady simulations.
| [in] | val_total_unsttimend | - Value of the non-dimensional total time. |
Definition at line 2782 of file CConfig.hpp.
| void CConfig::SetTotalTemperatureIn_BC | ( | su2double | val_temp | ) |
Set the inlet total temperature imposed as BC for internal flow.
| [in] | val_temp | - New value of the total temperature. |
Definition at line 9236 of file CConfig.cpp.
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Set the translational velocity of the mesh.
| [in] | iDim | - spatial component |
Definition at line 6004 of file CConfig.hpp.
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Set the value of the boolean for updating AoA in fixed lift mode.
| [in] | val_update | - the bool for whether to update the AoA. |
Definition at line 8776 of file CConfig.hpp.
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Set the value of the boolean for updating AoA in fixed lift mode.
| [in] | val_update | - the bool for whether to update the AoA. |
Definition at line 8770 of file CConfig.hpp.
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Set the free-stream velocity.
| [in] | val_velocity_freestream | - Value of the free-stream velocity component. |
| [in] | val_dim | - Value of the current dimension. |
Definition at line 2715 of file CConfig.hpp.
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Set the non-dimensional free-stream velocity.
| [in] | val_velocity_freestreamnd | - Value of the non-dimensional free-stream velocity component. |
| [in] | val_dim | - Value of the current dimension. |
Definition at line 2722 of file CConfig.hpp.
|
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Set the reference velocity for nondimensionalization.
| [in] | val_velocity_ref | - Value of the reference velocity. |
Definition at line 2546 of file CConfig.hpp.
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Set the freestream viscosity.
| [in] | val_viscosity_freestream | - Value of the freestream viscosity. |
Definition at line 2666 of file CConfig.hpp.
|
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Set the non-dimensional free-stream viscosity.
| [in] | val_viscosity_freestreamnd | - Value of the non-dimensional free-stream viscosity. |
Definition at line 2728 of file CConfig.hpp.
|
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Set the reference viscosity for nondimensionalization.
| [in] | val_viscosity_ref | - Value of the reference viscosity. |
Definition at line 2618 of file CConfig.hpp.
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Set the weight of objective function. There are several options: Drag coefficient, Lift coefficient, efficiency, etc.
Definition at line 5437 of file CConfig.hpp.
|
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Subtract one to the index of the finest grid (full multigrid strategy).
Definition at line 6331 of file CConfig.hpp.
| void CConfig::Tick | ( | double * | val_start_time | ) |
Start the timer for profiling subroutines.
| [in] | val_start_time | - the value of the start time. |
Definition at line 9776 of file CConfig.cpp.
| void CConfig::Tock | ( | double | val_start_time, |
| const string & | val_function_name, | ||
| int | val_group_id | ||
| ) |
Stop the timer for profiling subroutines and store results.
| [in] | val_start_time | - the value of the start time. |
| [in] | val_function_name | - string for the name of the profiled subroutine. |
| [in] | val_group_id | - string for the name of the profiled subroutine. |
Definition at line 9784 of file CConfig.cpp.
| bool CConfig::TokenizeString | ( | string & | str, |
| string & | option_name, | ||
| vector< string > & | option_value | ||
| ) |
breaks an input line from the config file into a set of tokens
| [in] | str | - the input line string |
| [out] | option_name | - the name of the option found at the beginning of the line |
| [out] | option_value | - the tokens found after the "=" sign on the line |
Definition at line 7745 of file CConfig.cpp.
| vector<string> CConfig::fields |
Tags for the different fields in a restart file.
Definition at line 1404 of file CConfig.hpp.
1.9.1